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Systems development life cycle (3,157 words) [view diff] no match in snippet view article find links to article

In systems engineering, information systems and software engineering, the systems development life cycle (SDLC), also referred to as the application development

second-generation satellites, improving accuracy, increasing power, extending the design life and adding the FDMA L2OF open signal. The last eight Glonass-M spacecraft

will be designed to provide protection for a specific lifetime, the 'design life' of the system, which may vary dependent upon the conditions encountered

Luxembourg government. It has a mass of 4,230 kg (9,330 lb) and has a design life of at least 15 years. The satellite was launched by SpaceX on 31 January

this was cancelled in late 2012 as the launch vehicle had exceeded its design life while in storage ahead of the launch. A total of 446 Kosmos 3Ms were

the series. The spacecraft have a mass of 1,633 kg (3,600 lb) and a design life of 12 years. Like earlier GPS satellites, Block IIF spacecraft operate

Airbus Defence and Space. It has a mass of 5,200 kg (11,500 lb) and has a design life of at least 15 years. The spacecraft had been ready to beam television

between Envisat and Sentinel-5. It was launched in October 2017, and has a design life of 7 years. The TROPOspheric Monitoring Instrument (Tropomi) provides

increased net power output of 1,000 MWe (1080 MWe gross) and a 60-year design life. The CPR-1000 is built and operated by the China General Nuclear Power

Boeing Satellite Systems. It has a mass of 2,302 kg (5,075 lb) and has a design life of at least 15 years. SES S.A. List of SES satellites "SES 15". Gunter's

markets. Intelsat 14 replaced Intelsat 1R which was at the end of its design life. It was built by Space Systems Loral, as part of its LS-1300 line. Intelsat

band transponders. Galaxy 18 replaced Galaxy 10R near the end of its design life. Galaxy 18 was launched on May 21, 2008. The launch took place successfully

600 kg (10,100 lb), a power production capacity of 8.5 kW and a 15-year design life. Its payload is composed of Ku band and Ka band transponders. SKY Perfect

market. Galaxy 19 replaced Galaxy 25 which is nearing the end of its design life and has been moved to 93.1°W longitude. It was built by Space Systems/Loral

tracking that is designed to be maintenance free over the twenty year design life of the system. The panels are mounted on a north-south axis and rotate

instrument from NASA. It has a mass of 4,423 kg (9,751 lb) and has a design life of at least 15 years. The launch of SES-14 on 25 January 2018 by an Ariane

market. Intelsat 11 replaced Intelsat 3R which was nearing the end of its design life. Intelsat 11 was built by Orbital Sciences Corporation, as part of its

and at launch it had a mass of 5,514 kilograms (12,156 lb). It has a design life of fifteen years. QuetzSat 1 is part of the SES satellite fleet. QuetzSat

geosynchronous orbit, at a longitude of 7° West. The spacecraft has a design life of 15 years and a mass at launch of 3.2 tonnes. It is powered by solar

a launch weight of approximately 1,645 kg (3,627 lb), and a 15-year design life. Its payload is composed of 1 C-band, and 20 S-band transponders and

featuring two deployable solar arrays with five panels on each. The design life is 15 years. The first satellite Kosmos 2520/Blagovest-11L was launched

width. Its development programme cost around 25 million rupee. It has a design life of one year. Jugnu was launched on 12 October 2011 into low Earth orbit

power production capacity of 9 to 9.9 kW at end of life and a 15-year design life. Its payload is composed of 26 C band and 18 Ku band transponders with

fuel assemblies. Other features include single containment, 40-year design life and a 12-month fuel cycle. The first CNP-600 unit began operation at

platform. It had a launch weight of 3,400 kg (7,500 lb), and a 10-year design life. Its payload is composed of 6 C-band, 11 Ka-band, 8 Ku-band and 1 S-band

panels, and instead relied on batteries for power. Early spacecraft had a design life of 33 days, including three in free flight, and the rest docked with

operates in slot 4 of plane A of the GPS constellation. The satellite has a design life of 10 years and a mass of 2,032 kilograms (4,480 lb). As of 2012 it remains

of the decision to end the use of steam traction by 1968, against a design life of over 30 years and a theoretical final withdrawal date of between 1990

USA-242 is a 1,630-kilogram (3,590 lb) spacecraft, built by Boeing with a design life of 15 years. It operates from a semi-synchronous medium Earth orbit,

use. It was decommissioned on 6 May 2011, two years into its ten-year design life. In addition to its operational navigation signals, USA-203 was also

platform. It had a launch weight of 3,400 kg (7,500 lb), and a 10-year design life. Its payload is composed of 6 C-band, 11 Ka-band, 8 Ku-band and 1 S-band

operates in slot 1 of plane A of the GPS constellation. The satellite has a design life of 15 years and a mass of 1,630 kilograms (3,590 lb). As of 2019 it remains

operates in slot 1 of plane C of the GPS constellation. The satellite has a design life of 10 years and a mass of 2,032 kilograms (4,480 lb). As of 2012 it remains

operates in slot 2 of plane D of the GPS constellation. The satellite has a design life of 15 years and a mass of 1,630 kilograms (3,590 lb). On 10 July 2023

operates in slot 2 of plane F of the GPS constellation. The satellite has a design life of 10 years and a mass of 2,032 kilograms (4,480 lb). As of 2015 it remains

panels have a span of 21.5 metres. It has three-axis stabilisation, and a design life expectancy of five years. The satellite became inoperable due to communications

constellation. The satellite has a mass of 2,032 kilograms (4,480 lb), and a design life of 10 years. As of 2012 it remains in service. "GPS 2R-15". US National

orbit at a longitude of 74 degrees east. At the end of its seven-year design life it was replaced by the newly launched INSAT-1D, dropping to backup status

constellation. The satellite has a mass of 2,032 kilograms (4,480 lb), and a design life of 10 years. As of 2019 it remains in service. "Navstar 59". US National

satellite bus. It had a launch weight of 4,820 kg (10,630 lb), a 15-year design life and was the first commercial communications satellite built in Japan

orbital position. The satellite failed on 4 July 2013, well short of its design life, for which RSCC collected the insurance. Ekspress-MD1 was a geostationary

990 lb) at launch, had a power production capacity of 15 kW and a 15-year design life. Its payload is composed of 61 Ku-band and 10 Ka-band transponders. Eutelsat

carried 38 IEEE C band and ten IEEE Ku band transponders, and had a design life of 13 years and a mass of 4,215 kilograms (9,292 lb). Following its arrival

carried 38 IEEE C band and ten IEEE Ku band transponders, and had a design life of 13 years and a mass of 4,296 kilograms (9,471 lb). During late 1991

constellation. The satellite has a mass of 2,032 kilograms (4,480 lb), and a design life of 10 years. The satellite was retired in 2018. "Navstar 50". US National

slot 5. The satellite has a mass of 2,032 kilograms (4,480 lb), and a design life of 10 years. It was originally retired on 23 June 2021. On 14 Aug 2023

QZS-1 (Michibiki-1) satellite launched in September 2010. QZS-1 has a design life of ten years. As QZS-1 is an experimental satellite, it did not broadcast

carried 38 IEEE C band and ten IEEE Ku band transponders, and had a design life of 13 years and a mass of 4,330 kilograms (9,550 lb). Upon entering service

constellation. The satellite had a mass of 2,032 kilograms (4,480 lb), and a design life of 10 years. USA-154 was initially retired on 9 July 2020. It was subsequently

constellation. The satellite has a mass of 2,032 kilograms (4,480 lb), and a design life of 10 years. As of 2019 it remains in service. "Navstar 57". US National

constellation. The satellite has a mass of 2,032 kilograms (4,480 lb), and a design life of 10 years. As of 2012 it remains in service. "Navstar 52". US National

safety systems and a 60-year design life.[citation needed] Generation II reactor designs generally had an original design life of 30 or 40 years. This date

Meteor-M No.1 was the designated replacement for Meteor-3M No.1, and had a design life of 5 years. In November 2014, Russian officials announced the termination

broadband across rural and remote Australia. Satellite Type: Hughes HS-376 Design Life: 7 Years for A1 & A2 - 10 Years for A3 Equipment: 15 Ku band transponders

constellation. The satellite has a mass of 2,032 kilograms (4,480 lb), and a design life of 10 years. It was decommissioned in January 2022, per the USCG Nanu

constellation. The satellite has a mass of 2,032 kilograms (4,480 lb), and a design life of 10 years. As of 2012 it remains in service. "Navstar 51". US National

itself to geostationary orbit using an IHI -500-N apogee motor. It has a design life of fifteen years, and carries thirty two J band transponders (US IEEE

orbit, most of the satellites re-entered before reaching their intended design life a week after launch. The first fully successful launch of Alpha took

400 kg (7,500 lb), a power production capacity of 10 kW and a 15-year design life. Its payload is composed of Ku band and Ka band transponders. SKY Perfect

on AMC-8 ended as of midnight 30 June 2017. Since AMC-8 is past its design life, it will soon be decommissioned. As of 1 July 2017, there are no plans

constellation. The satellite has a mass of 2,032 kilograms (4,480 lb), and a design life of 10 years. As of 2019 it remains in service. "Navstar 56". US National

constellation. The satellite has a mass of 2,032 kilograms (4,480 lb), and a design life of 10 years. As of 2012 it remains in service. "Navstar 54". US National

It is equipped with 17 C-band and 36 Ku-band transponders. It has a design life of 15 years. In February 2009, Gazprom ordered two Yamal-400 type satellites

constellation. The satellite has a mass of 2,032 kilograms (4,480 lb), and a design life of 10 years. As of March 2020 it is no longer in service. "Navstar 55"

construction, and the survival of some far longer than their original five-year design life combine to make them the subject of much continued interest. In 1936

with a 3 kilowatt solar array power capacity and sufficient fuel for a design life of twelve years. TMI Communications of Canada referred to its MSAT satellite

carried 38 IEEE C band and ten IEEE Ku band transponders, and had a design life of 13 years and a mass of 4,215 kilograms (9,292 lb). After launch, Intelsat

slot 2. The satellite has a mass of 2,032 kilograms (4,480 lb), and a design life of 10 years. As of 2019 it remains in service. GPS IIR-3 was originally

continued to operate for six months after launch. Orbital module data Design life: 200 days Length: 2.80 metres (9.2 ft) Basic diameter: 2.25 metres (7

and at launch it had a mass of 5,521 kilograms (12,172 lb). It has a design life of fifteen years,; however, it is carrying enough fuel for around twenty

bus designed for direct geostationary orbit injection with 14 years of design life. Its payload was supplied by Thales Alenia Space and is composed of 8

satellite bus. It is equipped with 46 Ku-band) transponders. It has a design life of 15 years, but reducing to 11 years expected after launch partial failure

transponders. At launch it had a mass of 6,258 kilograms (13,797 lb). It has a design life of fifteen years. It has a common configuration with EchoStar XI and

featured new upgraded flight control and power systems. Its official design life time was 5 years, up from 3 years for the most numerous Block IIv first

not taken out of service until 18 November 1995, well past its 5-year design life. The Block II satellites were the first full scale operational GPS satellites

DSCS-III satellite had a design life of ten years, although several of the DSCS satellites have far exceeded their design life expectancy. The mission

conditions around the world, greatly outliving its original three-year design life. Landsat 5 had a maximum transmission bandwidth of 85 Mbit/s. It was

provided navigation services within China. In December 2012, as the design life of BeiDou-1 expired, it stopped operating. The BeiDou-2 (second-generation

longwave thermal bands. The satellite was developed with a 5 years mission design life but was launched with enough fuel on board to provide for upwards of

Partial Test Ban Treaty went into effect, and the last in 1965. They had a design life of six months, but were only actually shut down after five years. Advanced

fuel assemblies. Other features include single containment, 40-year design life and a 12-month fuel cycle. The first CNP-600 unit began operation at

mass 40 to 45 kg (88 to 99 lb) Regime LEO, mostly 720 km × 720 km × 45° Design life 4 years Production Status Out of production Built 36 Launched 35 Operational

(design life: five years). The mission was judged as being successful by the involved scientists, in particular as the original 5 year design life was

mission was scheduled to last seven years, though the satellite had a design life of ten years. COMS-1 was deactivated on 31 March 2020, following a two-year

Smithsonian's Cooper Hewitt Design Museum, National Design Triennial 2006 “Design Life Now”, and he has spoken at the TED and 99U conferences about his career

Systems/Loral on the SSL 1300. It has a launch mass of 3,253 kg (7,172 lb) and a design life of more than 15 years. When stowed for launch, the satellite measures

weighs 1,413 kg (3,115 lb) generates 1000W of power and had a limited design life of 3 years, but it was extended to 5 years in later models. It had a

a mass of 2,630 kilograms (5,800 lb) at the beginning of its 15-year design life. When stowed for launch, it measured 5.7 metres (19 ft) of height and

(approximately 57 single area images) Spacecraft Fueled for 7 years, design life 5 years 2100 lb (950 kg), 3.04 m (10 ft) in length Launch Date: October

satellite bus. They have a mass of around 825 kilograms (1,819 lb), and a design life of 18–24 months. The satellites operate in low Earth orbits, typically

ultraviolet) wavelengths. Initially funded for two years, with a ten-year design life, the spacecraft remains in good health and has received repeated mission

Vidicon (RBV) and the Multispectral Scanner (MSS). Despite having a design life of one year, Landsat 2 operated for over seven years, finally ceasing

484 kg (5,476 lb) at launch, had a dry mass of 1,227 kg (2,705 lb), and a design life 15 years. It had a power availability dedicated to the payload of 4.6 kW

Systems, were 5.3 meters across with solar panels deployed, and had a design life expectancy of 5 years. Unlike the later operational satellites, GPS Block

orbit and will include two deployable solar arrays and batteries. The design life of the I-6F1 will be 15 years. The L-band payload supports Inmarsat's

has a mass of 5,282 kg (11,645 lb), produces 13 kW of power and has a design life of 15 years. It uses a hybrid approach for spacecraft propulsion, using

transponders, and at launch it had a mass of 3,112 kg (6,861 lb). It has a design life of fifteen years, however it was launched with enough fuel to operate

Corporation, at a cost of US$800 million each. Each satellite has a design life of 10 years. Six were built, of which five reached their operational

spacecraft measured 5.3 m across with solar panels deployed and had a design life of 7.5 years. USA-135 was launched at 00:30:00 UTC on 6 November 1997

spacecraft measured 5.3 m across with solar panels deployed and had a design life of 7.5 years. USA-128 was launched at 08:49:00 UTC on 12 September 1996

International for the Air Force Space Systems Division, each have a 7.5-year design life. The Air Force intends to launch a GPS II every 2 to 3 months until the

solely by NASA. Landsat 3 decommissioned on September 7, 1983, beyond its design life of one year. The data collected during Landsat 3's lifetime was used

3,105 kg (6,845 lb), a dry mass of 1,841 kg (4,059 lb) and a 12-year design life. When stowed for launch, its dimensions were 2.8 m × 4.9 m × 3.8 m (9 ft

spacecraft measured 5.3 m across with solar panels deployed and had a design life of 7.5 years. USA-87 was launched at 22:16:00 UTC on 18 December 1992

Systems, were 5.3 meters across with solar panels deployed, and had a design life expectancy of 5 years. Unlike the later operational satellites, GPS Block

spacecraft measured 5.3 m across with solar panels deployed and had a design life of 7.5 years. USA-79 was launched at 22:29:00 UTC on 23 February 1992

spacecraft measured 5.3 m across with solar panels deployed and had a design life of 7.5 years. USA-80 was launched at 03:20:00 UTC on 10 April 1992, atop

spacecraft measured 5.3 m across with solar panels deployed and had a design life of 7.5 years. USA-100 was launched at 03:40:01 UTC on 10 March 1994,

International for the Air Force Space Systems Division, each have a 7.5-year design life. The Air Force intends to launch a GPS II every 2 to 3 months until the

Systems, were 5.3 meters across with solar panels deployed, and had a design life expectancy of 5 years. Unlike the later operational satellites, GPS Block

spacecraft measured 5.3 m across with solar panels deployed and had a design life of 7.5 years. USA-63 was launched at 05:39:00 UTC on 2 August 1990, atop

orbit, the batteries are recharged. The nickel-hydrogen batteries had a design life of 6.5 years which means that they were replaced multiple times during

spacecraft measured 5.3 m across with solar panels deployed and had a design life of 7.5 years. USA-117 was launched at 00:21:00 UTC on 28 March 1996,

spacecraft measured 5.3 m across with solar panels deployed and had a design life of 7.5 years. USA-90 was launched at 03:09:00 UTC on 30 March 1993, atop

enough the surface soon becomes unsightly with rusting obvious. The design life is directly related to the metal coating thickness. Painting either by

spacecraft measured 5.3 m across with solar panels deployed and had a design life of 7.5 years. USA-64 was launched at 21:56:00 UTC on 1 October 1990,

spacecraft measured 5.3 m across with solar panels deployed and had a design life of 7.5 years. USA-54 was launched at 02:45:01 UTC on 26 March 1990, atop

International for the Air Force Space Systems Division, each have a 7.5-year design life. The Air Force intends to launch a GPS II every two to three months until

spacecraft measured 5.3 m across with solar panels deployed and had a design life of 7.5 years. USA-85 was launched at 23:54:00 UTC on 22 November 1992

702MP satellite bus. It has a launch mass of 6,600 kg (14,600 lb) and a design life of more than 15 years. When stowed for launch, the satellite measures

spacecraft measured 5.3 m across with solar panels deployed and had a design life of 7.5 years. USA-88 was launched at 02:55:00 UTC on 3 February 1993

International for the Air Force Space Systems Division, each have a 7.5-year design life. The Air Force intends to launch a GPS II every 2 to 3 months until the

spacecraft measured 5.3 m across with solar panels deployed and had a design life of 7.5 years. USA-126 was launched at 00:50:00 UTC on 16 July 1996, atop

Space Systems, were 5.3 m across with solar panels deployed, and had a design life expectancy of 5 years. Unlike the later operational satellites, GPS Block

Systems, were 5.3 meters across with solar panels deployed, and had a design life expectancy of 5 years. Unlike the later operational satellites, GPS Block

International for the Air Force Space Systems Division, each have a 7.5-year design life. The Air Force intends to launch a GPS II every 2 to 3 months until the

422 kg (11,953 lb) and 11 kW of payload power with over 15 years of design life. Its payload was also supplied by Thales Alenia Space and is composed

Space Systems, were 5.3 m across with solar panels deployed, and had a design life expectancy of 5 years. Unlike the later operational satellites, GPS Block

spacecraft measured 5.3 m across with solar panels deployed and had a design life of 7.5 years. USA-83 was launched at 09:20:01 UTC on 7 July 1992, atop

spacecraft measured 5.3 m across with solar panels deployed and had a design life of 7.5 years. USA-84 was launched at 08:57:00 UTC on 9 September 1992

Airbus Defence and Space. It has a mass of 5,384 kg (11,870 lb) and has a design life of at least 15 years. SES-12 was successfully launched on a SpaceX Block

The spacecraft continues to operate at Mars, far beyond its intended design life. Due to its critical role as a high-speed data-relay for ground missions

three cosmonauts to ISS and back Specifications Regime Low Earth orbit Design life Up to six months docked to ISS Production Status Retired (replaced by

W minimum Equipment Omnidirectional UHF radio Regime Low Earth orbit Design life 10 years Production Status Operational Built 12 Launched 12 Maiden launch

sport eight 130 watts Ku-band transponders (plus 4 spares), have a design life of 13 years and have a 1.8 kW power generation capability. It was expected

Systems, were 5.3 meters across with solar panels deployed, and had a design life expectancy of 5 years. Unlike the later operational satellites, GPS Block

England, since 1999, and still in production as of 2024. For part of their design life, Plaxton was part of TransBus International, during which time the designs

spacecraft measured 5.3 m across with solar panels deployed and had a design life of 7.5 years. USA-66 was launched at 21:39:01 UTC on 26 November 1990

spacecraft measured 5.3 m across with solar panels deployed and had a design life of 7.5 years. USA-71 was launched at 02:32:00 UTC on 4 July 1991, atop

spacecraft measured 5.3 m across with solar panels deployed and had a design life of 7.5 years. USA-92 was launched at 13:27:00 UTC on 26 June 1993, atop

spacecraft measured 5.3 m across with solar panels deployed and had a design life of 7.5 years. USA-91 was launched at 00:07:00 UTC on 13 May 1993, atop

spacecraft measured 5.3 m across with solar panels deployed and had a design life of 7.5 years. USA-91 was launched at 00:07:00 UTC on 13 May 1993, atop

span and ring protection and 1:n wavelength redundancy. The cable has a design life to 2026. Shima, Japan Maruyama, Chiba, Japan Tanguisson, Guam, unincorporated

an estimated launch mass of 3,500 kilograms (7,700 lb) with a 15-year design life. It has a single Ku-band payload with 24 transponders, and covers Japan

Systems, were 5.3 meters across with solar panels deployed, and had a design life expectancy of 5 years. Unlike the later operational satellites, GPS Block

Systems, were 5.3 meters across with solar panels deployed, and had a design life expectancy of 5 years. Unlike the later operational satellites, GPS Block

531 kg (7,785 lb) with a dry mass of 1,669 kg (3,680 lb) and a 13-year design life. As most satellites based on the A2100-AX platform, it uses a 460 N (100 lbf)

(JSAT). It had a launch mass of 2,906 kilograms (6,407 lb) and a 15-year design life. As most satellites based on the A2100 platform, it uses a 460 newtons

Systems, were 5.3 meters across with solar panels deployed, and had a design life expectancy of 5 years. Unlike the later operational satellites, GPS Block

bipropellant engine used for insertion into geostationary orbit. It has a design life of 15 years; however, it is fuelled for at least 16 years of operations

design to detailed design. Power output will be 1150 MWe, with a 60-year design life, and would use a combination of passive and active safety systems with

transponders, and at launch it had a mass of 6,180 kg (13,620 lb). It has a design life of fifteen years. It was launched on 14 February 2012, at 19:36:37 UTC

spacecraft measured 5.3 m across with solar panels deployed and had a design life of 7.5 years. USA-94 was launched at 12:38:00 UTC on 30 August 1993,

spacecraft measured 5.3 m across with solar panels deployed and had a design life of 7.5 years. USA-96 was launched at 17:04:00 UTC on 26 October 1993

Bus Astrobus Launch mass ~4 tonnes Regime 831 km Sun-synchronous orbit Design life 7.5 years Production Status Under Construction On order 6 Built 2 Launched

by body-mounted solar cells generating 183 watts of power. It had a design life of five years and carried an SVM-2 apogee motor for propulsion. Intelsat

courses in dance, drama, singing, writing, filmmaking, photography, art, design, life skills, & business training in venues across Central London. City Academy

adequate payload while being sufficiently reliable to safely fly for the design life of the aircraft. Similar to, but more exacting than, the usual engineering

(1998-2014) COSPAR ID 1994-064A SATCAT no. 23305 Mission duration 15 years design life Spacecraft properties Bus SSL-1300 Manufacturer Space Systems/Loral Launch

LSD is proportioned to sustain all actions likely to occur during its design life, and to remain fit for use, with an appropriate level of reliability

GAGAN navigation payload operating in L1 and L5 bands. GSAT-10, with a design life of 15 years was operational by November 2012 and will augment telecommunication

the mass of the satellite was 3,238 kilograms (7,139 lb). It has a design life of ten years. Power is supplied by a single gallium arsenide solar panel

proper staffing, risks, budget, and schedule. In NASA's engineering design life cycle, design reviews are held for technical and programmatic accountability

0 ft) Volume 9,000 cubic metres (320,000 cu ft) Regime Low Earth orbit Design life Up to 35 days Production Status No longer in service Launched 2 Maiden

Intelsat COSPAR ID 1993-066A SATCAT no. 22871 Mission duration 15 years design life Spacecraft properties Bus SSL-1300 Manufacturer Space Systems/Loral Launch

by body-mounted solar cells generating 183 watts of power. It had a design life of five years and carried an SVM-2 apogee motor for propulsion. Intelsat

Vehicle monitor Solid State camera(RS-D2) Regime 400km Circular Low Earth Design life 8 Production Status Retired Launched 4 Retired 2 Lost 2 Maiden launch

3G M5, which can be fabricated in China. Other features include has a design life that could extend beyond 40 years and an 18-month fuel cycle. It has

Intelsat COSPAR ID 1976-010A SATCAT no. 08620 Mission duration 7 years design life Spacecraft properties Bus HS-353 Manufacturer Hughes Communications Launch

Burst Retarded Potential Analyser[citation needed] Regime Low Earth Design life 2 years Production Status Retired Built 4 Launched 4 Retired 1 Lost 3

Ku-band physical transponders), the 6,010 kg (13,250 lb) satellite has a design life of 15 years. It is built on the Eurostar-3000 satellite bus. The SES-6

by body-mounted solar cells generating 183 watts of power. It had a design life of five years and carried an SVM-2 apogee motor for propulsion. Intelsat

for a year past the end of its design life. Its late entry into service was partly because GOES-10 exceeded its design life by over six years, and partly

proper engineering and testing protocols the FDR process provides a design life-cycle of 30 years. FDR is a manufacturing process and not an installation

operates in slot 6 of plane A of the GPS constellation. The satellite has a design life of 15 years and a mass of 1,630 kilograms (3,590 lb). It is currently

operates in slot 6 of plane D of the GPS constellation. The satellite has a design life of 15 years and a mass of 1,630 kilograms (3,590 lb). It is currently

Systems, were 5.3 meters across with solar panels deployed, and had a design life expectancy of 5 years. Unlike the later operational satellites, GPS Block

operates in slot 1 of plane E of the GPS constellation. The satellite has a design life of 15 years and a mass of 1,630 kilograms (3,590 lb). It is currently

continuously powered since it first became operational. Although the design life of the spacecraft avionics was only six months, the avionics systems

operates in slot 6 of plane F of the GPS constellation. The satellite has a design life of 12 years and a mass of 1,630 kilograms (3,590 lb). It is currently

Intelsat COSPAR ID 1978-002A SATCAT no. 10557 Mission duration 7 years design life Spacecraft properties Bus HS-353 Manufacturer Hughes Space and Communications

by body-mounted solar cells generating 183 watts of power. It had a design life of five years and carried an SVM-2 apogee motor for propulsion. Intelsat

Launch mass 1,700 kg (3,700 lb) Power 4 kW Regime Sun-synchronous orbit Design life 5 years (planned) Production Status Operational On order 4 Built 4 Launched

Accounting Business Studies Information Technology Engineering Graphics and Design Life Orientation Dramatic Arts Visual Communications Design Music Parel Vallei

mass of the satellite is about 3,500 kilograms (7,700 lb). It has a design life of 15 years with 8 years of operational life. Power is supplied by a

launch mass of 1,117 kg (2,463 lb), a geostationary orbit and a 7-year design life. On August 30, 1984, SBS 4 was launched by Space Shuttle Discovery in

Intelsat COSPAR ID 1978-035A SATCAT no. 10778 Mission duration 7 years design life Spacecraft properties Bus HS-353 Manufacturer Hughes Space and Communications

Crew capacity 3 Volume 45.00 m3 (1,589 cu ft) Regime low Earth orbit Design life 7 days Dimensions Length 13.2 m (43 ft) Diameter 4.15 m (13.6 ft) Maximum

/ NASA COSPAR ID 1971-109A SATCAT no. 5675 Mission duration 1 year (design life) Spacecraft properties Manufacturer BAC Launch mass 99.5 kilograms (219 lb)

Intelsat COSPAR ID 1975-091A SATCAT no. 08330 Mission duration 7 years design life Spacecraft properties Bus HS-353 Manufacturer Hughes Launch mass 1,515

Intelsat COSPAR ID 1975-091A SATCAT no. 08330 Mission duration 7 years design life Spacecraft properties Bus HS-353 Manufacturer Hughes Launch mass 1,515

1980s, the SSL 1300 platform underwent revision multiple times over its design life, all the while remaining a popular communications platform. The earliest

transponders (B-band / D-band) Data rate up to 64 kbit/s Regime Low Earth orbit Design life 5 years (planned) Production Status Active Related spacecraft Derived

Reconnaissance Specifications Bus Phoenix-Eye Regime Sun-synchronous Design life 2-4 years Production Status Operational On order 1 Built 15 Launched

transponders (NATO B / D band) Data rate of up to 64 kb/s) Regime Low Earth Design life 5 years Production Status Operational Related spacecraft Derivatives

Intelsat COSPAR ID 1995-013A SATCAT no. 23528 Mission duration 15 years design life Spacecraft properties Bus SSL-1300 Manufacturer Space Systems/Loral Launch

mission onset, approximately 1280 watts at the end of its seven-year design life. The payload housed 26 C-band and 6 Ku-band transponders. It could accommodate

satellite bus. It had a launch mass of 4,401 kg (9,703 lb) and a 12-year design life. It would provide communications services throughout Japan and Asia and

rated for 2000 hours of operation at 105 °C (221 °F), their expected design life roughly doubles for every 10 °C (18 °F) below this. At 65 °C (149 °F)

satellite bus. It has an estimated launch mass of 6 t (6.6 tons) and a design life of more than 15 years. It is powered by two wings, with four panels each

000 pounds (900 kg) and had 400 watts of power, 2000 detectors and a design life of 1.25 years. Throughout the life of the program, the satellite design

240 lb) Dimensions 3.4 × 1.8 × 2.35 m (11.2 × 5.9 × 7.7 ft) Power 1,700 W Design life 7 years Production Status Active Built 3 Launched 2 Operational 2 Maiden

launch, the satellite had a mass of 2,561 kg (5,646 lb). SES-1 has a design life of fifteen years; however, the spacecraft was launched with enough fuel

science, astrobiology Specifications Spacecraft type robotic aquatic rover Design life several months Dimensions Length 1 m (3 ft 3 in) Capacity Payload to

width. Its development programme cost around 1.5 crore rupee. It had a design life of one year, but is still working As of October 2017[update] and can

Applications Transport to low Earth orbit and back Specifications Regime Low Earth orbit Design life 1981 to 1991 Production Status Canceled, 1991 Launched None

Communications Operator Intelsat COSPAR ID INT4AF5 Mission duration 7 years (design life) Launch failure Spacecraft properties Bus HS-353 Manufacturer Hughes

eclipse, provided 1800 watts of power at mission onset of its seven-year design life. The payload housed 21 C-band and 4 Ku-band transponders. It could accommodate

Operator NASA Applications Bioscience Specifications Regime Low Earth orbit Design life 8-30 days Production Status Retired Launched 3 Maiden launch Biosatellite

operates in slot 3 of plane C of the GPS constellation. The satellite has a design life of 15 years and a mass of 1,630 kilograms (3,590 lb). It is currently

Intelsat COSPAR ID 1977-041A SATCAT no. 10024 Mission duration 7 years (design life) Spacecraft properties Bus HS-353 Manufacturer Hughes Space and Communications

3,150 kg (6,940 lb), a dry mass of 1,416 kg (3,122 lb) and a 13-year design life. When stowed for launch, it measured 4 m × 3.8 m × 2.4 m (13.1 ft × 12

operates in slot 5 of plane B of the GPS constellation. The satellite has a design life of 15 years and a mass of 1,630 kilograms (3,590 lb). It is currently

Management Process Process Assurance Certification Liaison Process Hardware Design Life Cycle Data Use of Previously Developed Hardware Commercial-Off-The Shelf

operates in slot 6 of plane E of the GPS constellation. The satellite has a design life of 15 years and a mass of 1,630 kilograms (3,590 lb). It is currently

1,500 kg (3,300 lb) after reaching geostationary orbit and an 8-year design life. When stowed for launch, its dimensions were 3.4 m (11 ft) long and 3

Intelsat COSPAR ID 1969-045A SATCAT no. 03947 Mission duration 5 years design life Spacecraft properties Manufacturer TRW Launch mass 647 kilograms (1,426 lb)

itself to geostationary orbit using a LEROS-1C apogee motor. It has a design life of fifteen years, and carries forty two transponders; twelve G/H band

1972-stock trains on the Bakerloo line have already exceeded their original design life of 40 years. London Underground is therefore extending their operational

Group COSPAR ID 2008-063A SATCAT no. 33453 Mission duration 16 years (design life) Spacecraft properties Bus Spacebus 4000C4 Manufacturer Thales Alenia

mission onset, approximately 1280 watts at the end of its seven-year design life. The payload housed 26 C-band and 6 Ku-band transponders. It could accommodate

launched in May 1999 along with Shijian-5, also completed its two-year design life operating until January 2004. The last satellite of the class, FY-1D

Asia region. The satellite relies on the SSL 1300 satellite bus with a design life of 16 years with up to 21 years of fuel remaining. The development of

this was cancelled in late 2012 as the launch vehicle had exceeded its design life while in storage ahead of the launch. The Kosmos-3MR rocket (GRAU Index:

Intelsat COSPAR ID 1994-034A SATCAT no. 23124 Mission duration 15 years design life Spacecraft properties Bus FS-1300 Manufacturer Space Systems/Loral Launch

mission onset, approximately 1280 watts at the end of its seven-year design life. The payload housed 29 C-band and 6 Ku-band transponders. It could accommodate

by a Start-1 launch vehicle. It had a mass of 317 kg (699 lb) and a design life of 3 years (fuel reserves for 5 years). It included a panchromatic (black-and-white)

carried 38 IEEE C band and ten IEEE Ku band transponders, and had a design life of 13 years and a mass of 4,215 kilograms (9,292 lb). Upon arrival in

1,700 kg (3,700 lb) and requiring up to 3 kW of power. Its expected design life is 6 to 15 years and has a 21 to 36 month to delivery lead time. GEOStar-1:

engine. As a cruise-missile expendable powerplant the Soar engine had a design life of 10 hours for a Red Rapier flight time of about 1 hour (range 400 nautical

operates in slot 5 of plane F of the GPS constellation. The satellite has a design life of 12 years and a mass of 1,630 kg (3,590 lb). It is currently in service

1,317 kg (2,903 lb), a dry mass of 535 kg (1,179 lb), and a 10-year design life. As all four STAR-1 satellites, it had a solid rocket Star 30CBP apogee

Intelsat COSPAR ID 1995-023A SATCAT no. 23571 Mission duration 15 years design life Spacecraft properties Bus SSL-1300 Manufacturer Space Systems/Loral Launch

maintenance and thermal control-environmental containment". Although the design life of the spacecraft avionics was only six months, the avionics systems

Kazakhstan. The satellite has a mass of 120 kilograms (260 lb) and a design life of five years. It carries a multi-spectral imager with a resolution of

Crewed flight launching with two cosmonauts, remained in orbit past design life due to Soyuz 33 failure, returned to Earth uncrewed 27 February 15:00

Intelsat COSPAR ID 1995-001A SATCAT no. 23461 Mission duration 15 years design life Spacecraft properties Bus SSL-1300 Manufacturer Space Systems/Loral Launch

With fuel, its mass is 1,982 kilograms (4,370 lb). The spacecraft has a design life of 12 years. The satellite carries six Ku-band and six Extended C-band

EchoStar COSPAR ID 2003-034A SATCAT no. 27854 Mission duration 12 years (design life) Spacecraft properties Spacecraft FS-1300 Manufacturer Space Systems/Loral

celebrate 35 years of continuous operation since launch. Its original design life expectancy was only 6 months. Although NASA described Pioneer 6 as "extant"

geostationary orbit. In July 2017, seven years past its 12-year intended design life, NSS-806 lost the use of 12 of its 39 transponders. NSS-806's replacement

satellite exceeded expectations by operating well past its one year design life. Spaceflight portal 1993 in spaceflight "ALEXIS 3rd Year Anniversary

(ORUs). ORUs are parts that can be replaced when they fail or pass their design life, including pumps, storage tanks, antennas, and battery units. Such units

satellite bus. It had a launch mass of 4,528 kg (9,983 lb) and a 15-year design life. As most satellites based on the A2100 platform, it uses a 460 N (100 lbf)

cells, batteries Equipment S-Band transceiver Regime Low Earth Orbit Design life 1 year Production Status In Service Built 4 Launched 4 Operational 4

mission onset, approximately 1280 watts at the end of its seven-year design life. The payload housed 26 C-band and 6 Ku-band transponders. It could accommodate

location: 79° West Launch Date: 28 October 1998 Vehicle: Ariane 44L Design life: 15 years Band: Ku-band Ku-band payload: 16 x 54 MHz Transponder type:

an estimated launch mass of 3,530 kilograms (7,780 lb) with a 15-year design life. It will have a single Ku-band payload with 24 transponders. It will

905 lb), the largest Intelsat's currently active satellite, and has a design life of more than 15 years. It is powered by two wings, with four solar panels

1,275 kg (2,811 lb), a dry mass of 535 kg (1,179 lb), and a 10-year design life. As all four STAR-1 satellites, it had a solid rocket Star 30CBP apogee

GPS satellite. The satellite has a mass of 2,032 kg (4,480 lb), and a design life of 10 years. As of 2012 it remains in service. "Navstar 47 2000-025A"

for a significant portion of the time and energy expended in the chip design life cycle, often quoted as 70%. With the growing complexity of chips, hardware

mission onset, approximately 1280 watts at the end of its seven-year design life. The payload housed 26 C-band and 6 Ku-band transponders. It could accommodate

congestion. It was constructed during 1971–72, but with only a 40-year design life as it was expected to be redundant once the planned Beechboro–Gosnells

Station that can be readily replaced when the unit either passes its design life or fails. ORUs are parts of the main systems and subsystems of the external

coatings. In some cases, such as very aggressive environments or long design life, both zinc and a coating are applied to provide enhanced corrosion protection

Australia to provide telephony services connected to the world, with a design life of 25 years and at a cost of A$160 million. The name was derived from

May 2009, more than 19 years after launch and 13 years beyond their design life. Because of its simple atomic structure, consisting only of a proton

1,317 kg (2,903 lb), a dry mass of 927 kg (2,044 lb), and a 10-year design life. As all four STAR-1 satellites, it had a solid rocket Star 30CBP apogee

Intelsat COSPAR ID 2007-016B SATCAT no. 31307 Mission duration 15 years (design life) Spacecraft properties Bus Spacebus 3000B3 Manufacturer Alcatel Alenia

correction methods. Errors can be predicted using surface error scanning. The design life is from 20 to 100 years, depending on the quality of the discs, the quality

Applications Space station logistics Specifications Regime Low Earth Design life 180 days Production Status Retired Built 11F615A55: 67 11F615A60: 29

council's offices at the civic centre were deemed to be at the end of their design life. The council purchased an existing building called Plaza West on Bridge

satellite bus. It had a launch mass of 4,048 kg (8,924 lb) and a 15-year design life. It would provide communications services throughout Japan and Asia.

further ₹1.11 billion (US$13 million) to launch. The satellite had a design life of five years. The satellite was used for natural resources management

launch mass of 550 kg (1,210 lb), a geostationary orbit and a 7-year design life. On September 24, 1981, SDS 2 was finally launched by a Delta-3910 PAM-D

replaces Intelsat 907, a 17-year-old satellite now four years past its design life. After five years, MEV-1 will move Intelsat 901 back to a final graveyard

Navigator Launch mass 1,764 kilograms (3,889 lb) Power 1,800 W Regime GEO Design life 10 years Production Status In Production Built 4 Launched 4 Operational

the ring road and beyond, an eight-lane carriageway was planned with a design life of 20 years. The conclusion was to develop a highway with access control

average) Quantization 12 bits Spatial resolution 250 m (bands 1–2) 500 m (bands 3–7) 1000 m (bands 8–36) Temporal resolution 1–2 days Design life 6 years

OKB-1 Applications Bioscience Specifications Regime Low Earth orbit Design life 5-22 days Production Status Retired (Bion-M in service) Launched 11 Maiden

estimated battery life is 700 cycles at 80% depth of discharge and the design life is 12 years. The cost per mile is estimated at between 1p and 1.2p depending

satellite bus. Fully fueled, it has a mass of 3,454 kg (7,615 lb), with a design life of 15 years. It carries two steerable antennas capable of providing S

constellation. The satellite has a mass of 2,032 kg (4,480 lb), and a design life of 10 years. As of 2023[update] it remains in service and holds the record

capacity 250 kg (550 lb) Power 400 W from a single solar array on a boom Design life 1 lunar day (14 Earth days) Dimensions Length Height: >2 m (6 ft 7 in)

Accommodation) Act 1944 led to the building of prefab bungalows with a design life of ten years. Innovative steel-framed properties were also tried in an

spans 42 Load limit 15 t (15,000 kg) No. of lanes 2 to 4 (1 to 2 per direction) Design life 4 to 13 years History Construction end 1998 (all bridges)

at an unnecessary cost. The mass in kg is given by equation (5). The design life is in years (1 year = 8760 hours). The utilisation factor (UF) of the

the use of commercial off-the-shelf equipment. The spacecraft has a design life of one year, and its Solar panels will provide it with at least 1,300

satellite bus. The satellite has a mass of 6,168 kg (13,598 lb) and a design life of 14 years. It will be used to provide super high frequency (SHF) and

Dimensions 3.710 × 2.202 × 2.207 m (12.2 × 7.2 × 7.2 ft) Power 2,100 W Design life 7 years Production Status Active On order 2 Built 2 Launched 2 Operational

satellite bus. Fully fueled, it has a mass of 3,454 kg (7,615 lb), with a design life of 15 years. It carries two steerable antennas capable of providing S

that time, much of the Region's slam door fleet reached the end of its design life of 35–40 years and was replaced by more reliable sliding- and plug-door

satellite bus. It had a launch mass of 4,007 kg (8,834 lb) and a 15-year design life. A near copy of JCSAT-3A, it was to be used as an on orbit spare. As

3,600 kg (7,937 lb) Dimensions 2.280 × 2.760 × 5.170 m (7.5 × 9.1 × 17.0 ft) Power 2,000 W Design life 8.5 years Production Status Under construction

0 ft) Longest span 104 m (341.2 ft) Clearance below 8.9 m (29.2 ft) Design life Modern bridge (1971–present) Victorian stone arch (1832–1968) Medieval

low volume roads not subject to heavy loading typically have a short design life; therefore minor loss of performance is tolerable. However, in critical

sensing Specifications Bus Phoenix-Eye 1 Regime Sun-synchronous orbit Design life 2-3 years Production Status Operational On order 1 Built 6 Launched 6

cosmonauts to Mir and ISS and back Specifications Regime Low Earth orbit Design life Up to six months docked to station Production Status Out of service Launched

LCU fleet as a similarly rugged steel craft (to the LCU 1610) with a design life of 30 years. The similarities of these two classes of ships will help

launch mass of 550 kg (1,210 lb), a geostationary orbit and a 7-year design life. On November 15, 1980, SBS 1 was launched by a Delta-3910 PAM-D from

designed by Mott, Hay and Anderson, built by Balfour Beatty, and has a design life of at least 100 years. During construction of the tunnel a problem was

developed at the Chinese Academy of Space Technology (CAST) and had a design life 4.5 years. The first operational satellite in this group was launched

launch it had a mass of approximately 4,635 kilograms (10,218 lb), with a design life of 15 years. Its 34-metre (112 ft) solar arrays will generate a minimum

Porsche 914 and Boxster, Toyota MR2 and Fiat X1/9. Sometimes during the design life of the vehicle, the lid may be restyled to increase the size or improve

early versions and up to 550 in later models. The 747SR had an economic design life objective of 52,000 flights during 20 years of operation, compared to

(indicating a problem with Astra 3B, which still had some two years of its design life remaining) and Astra 5B was renamed Astra 3C. Spaceflight portal Astra

(13 ft × 8.5 ft × 8.2 ft) Power 5.9 kilowatts (5,900 W) Batteries 324 Ah Design life 7 years (12 years of consumables) Production Status Active On order 4

continued to provide full service for 14 years; two years longer than its design life of 12 years. On March 26, 1996, another catastrophic failure occurred

generate around 12 kilowatts of power at the beginning of the satellite's design life, and around 11 kilowatts at the end of it. Arabsat-5A was launched by

has a mass of 6,411 kg (14,134 lb), produces 15 kW of power and has a design life of 15 years. Like all SpaceBusNEO, SES-17 uses electric propulsion exclusively

1,000 kg (2,200 lb) Crew capacity 4 Dimensions Height: 14 m (46 ft) Design life ≈ 10 flights Production Status Proposed Related spacecraft Flown with

satellite bus. The satellite has a mass of 6,168 kg (13,598 lb) and a design life of 14 years. It will be used to provide super high frequency (SHF) and

800 lb), with 1.5 kilowatts of power provided by three solar panels. Its design life was seven years. IKONOS operated in a Sun-synchronous, near-polar, circular

intermediate-power variant of the SSL 1300 satellite bus with a 15+ year design life. Coupled with the boost provided by its Falcon 9 launch vehicle, it carries

(357 lb) Power 85 watts Equipment 2 transponders Regime Geostationary Design life 3 years Production Status Retired Built 4 Launched 4 Retired 4 Maiden

instructions for fast FPU context save and restore. Towards the end of its design life, Deschutes chips capable of 500 MHz within Intel cooling and design specifications

ensure that such structures can endure such loading for their entire design life without failing. These works can require mechanical structural engineering:

design to detailed design. Power output will be 1150 MWe, with a 60-year design life, and would use a combination of passive and active safety systems with

satellite bus. The satellite has a mass of 6,168 kg (13,598 lb) and a design life of 14 years. It will be used to provide super high frequency (SHF) and

2011. Launched on the Long March 3B launch vehicle, the satellite has a design life of 15 years with initial goals to provide broadband internet access,

started an LCAC Service Life Extension Program (SLEP) to add 10 years of design life to each craft. The SLEP will be applied to 72 LCACs, extending their

Specifications Bus GRAU: 71Kh6 Launch mass 2600 Regime Geosynchronous Design life 5-7 years Production Status Out of production Launched 8 Operational

orbit, Medium Earth orbit (circumlunar spaceflight during early program) Design life Up to 6 months (docked to International Space Station) Production Status

Cargo Payload capacity 2,400 kg (5,300 lb) Volume 7.6 m3 (270 cu ft) Design life 180 days docked to a space station Dimensions Length 7.23 m (23.7 ft)

Crew capacity Up to 7 Volume 11 m3 (390 cu ft) Regime Low Earth orbit Design life 60 h (free flight) 210 days (docked) Dimensions Length 5.03 m (16.5 ft)

than those used in traditional lamps. The design life of the bulb is approximately 60,000 hours. The design life of the magnetron has been improved by the

BSS-702HP satellite bus. It has a mass of 5,987 kg (13,199 lb) and a design life of fourteen years. Its two solar panels generate upwards of 11 kW of

Design - Madame de Sade 2010: WhatsOnStage Award for Best Lighting Design - Life is a Dream 2010: LA Stage Alliance Ovation Awards - Parade 2010: LDI

Guárico state by Venezuela's Bolivarian Agency for Space Activities, design life span (5 years) The satellite was launched 9 October 2017 at 4:12 UTC

airspeed is Mach 0.85 (488 kn; 903 km/h; 561 mph). The aircraft has a design life of 44,000 flight cycles. Among 787 flight systems, a key change from

m long × 15.7 m wide Stowed size: 19.7 m long × 4.57 m wide Mission design life: 20 years Launch date: 2017 Launch Vehicle: Delta IV Heavy Cost: 16 billion

concerns or incident. Many reactors are closed long before their license or design life expired and are decommissioned. The costs for replacements or improvements

satellite bus. The satellite has a mass of 6,168 kg (13,598 lb) and a design life of 14 years. It will be used to provide super high frequency (SHF) and

JSTOR 1937181. Eliahu Zahavi, Vladimir Torbilo & Solomon Press (1996) Fatigue Design: Life Expectancy of Machine Parts. CRC Press. ISBN 978-0-8493-8970-2. Sutherland

base diameter Power 6 solar panels + batteries Regime Molniya orbit Design life 1.5 to 5 years Production Status Retired Launched 164 Maiden launch Molniya

cars, with a design speed of 80 km/h (50 mph), VVVF AC drive, and a design life of 30 years. 12A01 train 12A02 train being hauled "Metro breaks records"

concessions. Ducati argued that the current engine was at the end of its design life (which surrendered as much as 20 hp to the competition in 2007, its last

satellite bus, Hot Bird 6 is a 3,905 kg (8,609 lb) satellite with a design life of 12 years. It is equipped with an S400-12 apogee motor which was used

to its systems, generating 2,300 watts of electrical power, and had a design life of three years. The CBERS-3 spacecraft carried four instruments: MUXCam

the surviving First Generation units were reaching the end of their design life, leading to spiralling maintenance costs, poor reliability and a poor

Applications Space station logistics Specifications Regime Low Earth Design life 6 months Production Status Retired Built 11F615A55: 11 11F615A70: 0 Launched

its systems, generating 2,300 watts of electrical power, and have a design life of three years. The CBERS-4 spacecraft carries four instruments: MUXCam

Multispectral array detectors Steerable antenna Regime Geostationary orbit Design life 7 years (planned) Production Status Planned Launched 1 Operational 0

Engineering, Fabrication & Installation 2002 50,000 lb. Doors with 300-year design life Dynamics Research US Army Training Simulator Fabrication 2006 Simulator

recirculating cooling water systems. With the exception of machines with short design life, closed recirculating systems require periodic cooling-water treatment

provide communications to Asia and Australia. Palapa-D was built with a design life of fifteen years, but due to the expenditure of fuel during maneuvers

cars, with a design speed of 80 km/h (50 mph), VVVF AC drive, and a design life of 30 years and are China's first domestically developed trains. Trains

Flxible "New Looks" purchases in 1969, reached the end of their 12-year design life and funds for their replacement were not available. Most of the rest

satellite bus. At launch it had a mass of 1,244 kg (2,743 lb), and a design life of thirteen years. It carried twenty four C-band transponders. After

106.35 ft (32 m) Height 65 ft (20 m) No. of spans 11 No. of lanes 4 Design life 75 years History Constructed by PCL Construction Construction start August

brought by Space Shuttle missions. The nickel-hydrogen batteries had a design life of 6.5 years and could exceed 38,000 charge/discharge cycles at 35% depth

mass of 2,460 kg (5,420 lb) a power production of 3.7 kW and an 11-year design life. Stowed for launch it measured 3.6 m × 2.7 m × 4.3 m (11.8 ft × 8.9 ft

L1SF, L2OF and L2SF CDMA signals: L3OC Regime Medium Earth orbit (MEO) Design life 10 years (planned) Production Status In production On order 7 Built 5

Specifications Launch mass 1,000 kilograms (2,200 lb) Regime Low Earth Design life 3-5 years Production Status In production On order 4 Built 3 Launched

would be 60-70 years old at the time of replacement, around twice their design life. Since the withdrawal of the final Class 483 trains on the Isle of Wight

satellite bus. The satellite has a mass of 6,168 kg (13,598 lb) and a design life of 14 years. It will be used to provide super high frequency (SHF) and

with glulam and steel construction and had been erected in 2012, with a design life of "at least 100 years". The cause of the failure was not immediately

28–32-volt, 296 ampere hour silver-zinc Regime Lunar orbit Lunar landing Design life 75 hours (extended) Dimensions Length 23 ft 1 in (7.04 m) Diameter 13 ft

Production Design Won 1997 Marianna Ucrìa Nominated 1998 Best Costume Design Life Is Beautiful Nominated Best Production Design Nominated 2003 Best Costume

February 2020, after 17 years of operation (over three times the original design life of five years). The spacecraft had struggled with battery degradation

new and many of the quickly built houses have reached the end of their design life. The masterplans dictated low density development with large amounts

mounted on booms, and 2560 solar cells provided 30 Watts of power. Its design life-span was eight months owing to the low planned orbit.: 423  The satellite

DARPA COSPAR ID 1994-046A SATCAT no. 23191 Mission duration 1 year (design life) 3 years (target) 22 months (achieved) Spacecraft properties Bus PegaStar

land mobile service, and television and radio programming. Each had a design life of 7 years and a bandwidth of 72 MHz. ECS-3 was lost in an Ariane 3 launch

in launches through 2005, a total of 56 satellites were launched. The design life was three years, however numerous spacecraft exceeded this, with one

participating countries through peer review of submitted proposals. ROSAT had a design life of 18 months, but was expected to operate beyond its nominal lifetime

safety limits. It uses a simpler fueling procedure and has an extended design life of 60 years. Safety enhancements include the elimination of outer primary

500 kg) Crew capacity 4–6 Volume 18 m3 Regime LEO, TLI, Lunar orbit Design life Planned: 5–30 days (free flight) 365 days (docked in LEO) 200 days (docked

deployed Volume 5 m3 Power N2O4/UDMH Batteries Equipped Regime Lunar orbit Design life 48 hours Production Status Canceled Built Several Launched 3 (T2K) Failed

620 watts (solar array) Lander: 70 watts (two RTG units) Regime Areocentric Design life Orbiters: 4 years at Mars Landers: 4–6 years at Mars Production Status

runway was previously resurfaced in 1999 with a surface material having a design life of between 12 and 15 years. A major patch and repair was undertaken on

230 μm. While Herschel's dependence on liquid helium coolant limited the design life to around three years, SPICA would have used mechanical Joule-Thomson

2022 Tim Hatley (set design), Nick Barnes and Finn Caldwell (puppet design) Life of Pi Tim Hatley (set design) and Finn Ross (video design) Back to the

communications. All DSCS III satellites have exceeded their 10-year design life. The National Science Foundation use the DSCS satellites to provide additional

Misérables The Master A Royal Affair Best Cinematography Best Costume Design Life of Pi – Claudio Miranda Anna Karenina – Seamus McGarvey Beasts of the

signed an order to do so. By this stage Mir was well past the end of its design life, and Roscosmos General Director Yuri Koptev believed that "any of its

Specifications Bus Yantar (satellite) Launch mass 6,570 kg (14,480 lb) Regime SSO Design life 5 years Production On order 1 Built 4 Launched 4 Operational 3 Retired

Force COSPAR ID 1993-041A SATCAT no. 22698 Mission duration 3 year (design life) Spacecraft properties Launch mass 89.3 kilograms (197 lb) Start of mission

cost of $185.5 million, and have the following specifications: 100-year design life Length: 2,593 feet (790 m) Width: varies between 45 and 66 feet (14 and

(Robin Joseph and Kim Leow) In a Heartbeat (Ringling College of Art and Design) Life Smartphone (Central Academy of Fine Arts) Lost Property Office (Daniel

2014-07-31. Ryoko. "Sento Art: Public Bath House Paintings | PingMag : Art, Design, Life – from Japan". Pingmag.jp. Retrieved 2014-07-31. "Please enjoy Japanese

Spaceplane Launch mass 21,000 kg (46,000 lb) Payload capacity 3,000 kg (6,600 lb) Crew capacity Three Design life 30 to 90 days Production Status Cancelled

satellite bus. It had a launch mass of 2,982 kg (6,574 lb) and a 12-year design life. Its solar panels span 21 m (69 ft) when fully deployed and generated

the INSAT-4CR was placed in its slot. Satellite completed its planned design life while it was fully operational. ISRO claims this GSLV flight to be successful

December 2021). "South Africa's SumbandilaSat Reaches the End of its Design Life". Space in Africa. Retrieved 21 December 2021. The Official SumbandilaSat

Environment Agency was examining the Thames Barrier for its potential design life under climate change, with early indications being that subject to appropriate

to 1,740 lb) after reaching geostationary orbit and an 8 to 10-year design life. When stowed for launch, its dimensions were 2.8 to 3.15 m (9 ft 2 in

mass 3,400 kg Payload capacity 3,000 kg Volume 18.9 m3 Power 3.5 kW Design life 1 week to 2 years Dimensions Length 5.1 m Diameter 3.07 m Production

width. Its development programme cost around 25 million rupees. It has a design life of one year. Jugnu's primary instrument is the Micro Imaging System,

minutes, and the Venera 14 lander for 57 minutes, where the planned design life was only 32 minutes. The Venera 14 craft had the misfortune of ejecting

satellite was conducted using the 3-axial method (zero momentum), and design life was five years. The TV transponder units are designed to sufficiently

percent of the required power was available. The spacecraft, with a design life of seven years, operated successfully for 11 years, providing 60 channels

satellite bus. At launch, it had a mass of 3,379 kg (7,449 lb), and a design life of thirteen years. It carries twenty six C-band and eight Ku-band transponders

apparatus – Influence of the interaction between the user and the equipment on design Life-support equipment – Equipment which is necessary to support life in a

of 723 kg (1,594 lb) after reaching geostationary orbit and a 10-year design life. When stowed for launch, its dimensions were 3.15 m (10.3 ft) long and

702MP satellite bus. It has a launch mass of 6,552 kg (14,445 lb) and a design life of more than 15 years. When stowed for launch, the satellite measures

Unpressurised: 1.75 t Volume Pressurised: 78 m3 (2,800 cu ft) Power 3 kW Design life 6 months (berthed to ISS) / 1.5 years (after departure from ISS) Production

on-board fuel remaining to allow it to exceed its specified 13-year design life. Telesat launched Telstar 12 Vantage in November 2015 on a H2A204 variant

1,364 kg (3,007 lb) after reaching geostationary orbit and an 8-year design life. When stowed for launch, its dimensions were 3.4 m (11 ft) long and 3

orbit. The satellite lasted 11 years and 2 months, a bit short of the design life of 12 years. Right after solar panel deployment Yamal-101 failed irreparably

316 cu ft (9 m3) Power Solar Regime Lunar Transfer Orbit, lunar orbit Design life 21.1 days Dimensions Length 10 feet 10 inches (3.30 m) Diameter 16 feet

inclination of 57deg which did not provide full Earth coverage. It had a design life of two years, with a goal of three, but lasted 21 years suffering several

building became operational. This terminal building was planned for a design life of 10 years, until completion of the planned new permanent facility.

3,105 kg (6,845 lb), a dry mass of 1,841 kg (4,059 lb) and a 12-year design life. When stowed for launch, its dimensions were 2.8 m × 4.9 m × 3.8 m (9 ft

indices Edible packaging Ecodesign Reusable shopping bag Sustainable Design Life Cycle Assessment Wood, Marcia (April 2002). "Leftover Straw Gets New

visitors' centre is also planned for the barrage. The barrage has a design life of 120 years. The project also included the regeneration of 100 ha of

Pontifical Faculty of Theology of Sardinia and of the European Institute of Design. Life expectancy in Cagliari is high: 79.5 years for men and 85.4 for women

preserved and remains a witness to the ability of an American automaker to design life saving safety systems into cars without a government mandate. Notably

conducted while wearing hazmat protective clothing. The engine has a design life of 8,650 total accumulated cycles, with inspection and overhaul of the

when the trains would be 60 to 70 years old — probably double their design life. Since the withdrawal of the Class 483 on the Isle of Wight, the 1972-stock

sound levels emitted when the vehicle is engaged in lower gears. The design life of the lower ratio gears is shorter, so cheaper gears may be used, which

kilograms (99 lb) Equipment SHF 7–8 GHz transponder Regime Subsynchronous Design life 6 years Production Status Retired Launched 35 (8 launch failures, 27

of aspects fall outside current standards. The bridge has a 120-year design life. The bridge is a dual, tied arch bridge or bowstring bridge. It has a

and water vapor content, a first for the GRACE mission. GRACE-FO has a design life of 5 years. Spaceflight portal Challenging Minisatellite Payload (CHAMP)

land mobile service, and television and radio programming. Each had a design life of 7 years and a bandwidth of 72 MHz. ECS-3 was lost in an Ariane 3 launch

likely 4 to 15 years but the design life should be as long as possible: at least 10 years is desirable. The longer the design life, the longer the interval

Power Solar Regime Low Earth orbit, lunar Transfer Orbit, lunar orbit Design life 21 days Dimensions Length Total length: 7.23 metres (23.7 ft) (LEO configuration)

would only be problematic if experienced many times over a vehicle's design life). Since the gap fillers are not necessary for re-entry, it was acceptable

Batteries Nickel–hydrogen battery Regime Semi-synchronous Medium Earth orbit Design life 15 years (planned) Production Status Production complete On order 0 Built

has identified 224 bridges along Acela's route that are beyond their design life. South of the Delaware River, the Acela's top speed is 135 mph (217 km/h)

kilograms (4,540 lb), a dry mass of 975 kilograms (2,150 lb), and a 15-year design life. As most satellites based on the A2100 platform, it uses a 460 newtons

rate, and rate of precession.: 423  OV3-3 massed 75 kg (165 lb). Its design life-span was one year.: 423  OV3-3's scientific payload consisted of seven

ampere-hour silver-oxide Regime Low Earth orbit Cislunar space Lunar orbit Design life 14 days Dimensions Length 36.2 ft (11.0 m) Diameter 12.8 ft (3.9 m) Production

much of the play equipment demolished as it had reached the end of its design life. The playground reopened in October 2021 with a larger, updated design

Four-Year: Arts, Music & Design Schools not-for-profit --- --- Arts & design Life Pacific University San Dimas Los Angeles 1923 Special Focus Four-Year:

Specifications Launch mass 7,000 kilograms (15,000 lb) Regime Sun-synchronous Design life 3-5 years Production Status In production Built 3 Launched 3 Operational

and rate of precession.: 423  OV3-1 massed 69 kilograms (152 lb) Its design life-span was one year.: 423  OV3-1 carried six AFCRL experiments that had

3 Volume 10.5 m3 (370 cu ft) Batteries 755 Ah Regime Low Earth orbit Design life 210 days when docked to International Space Station (ISS) Dimensions

Crews and pressurized as well as unpressurized logistics Regime LEO Design life 10 days (free flight) 210 days (docked to ISS)[better source needed]

mounted on booms, and 2560 solar cells provided 30 Watts of power. Its design life-span was eight months owing to the low planned orbit.: 423  The satellite

Godavari Arch Bridge Characteristics Total length 2.7 kilometres (1.7 mi) Design life 100 years History Construction start 11 November 1897 (1897-11-11) Opened

kilometres (34 mi) No. of spans 3 No. of lanes 3 lanes per direction Design life 120 years History Construction start 15 December 2009; 14 years ago (2009-12-15)

long with 125 m between abutments. The bridge was opened in 1981 with a design life of 120 years. Geotechnical surveys prior to construction had indicated

land mobile service, and television and radio programming. Each had a design life of 7 years and a bandwidth of 72 MHz. ECS-3 was lost in an Ariane 3 launch

OPR-1000, the key features are: Net Electric power: 1400 MW (40% increase) Design Life: 60 years (50% increase) Seismic Design Basis: 0.3g (50% increase) Core

previous satellite, OPUSAT, which was launched in 2014. OPUSAT-II had a design life of five and a half months. OPUSAT-II had two main missions. The first

cross-tail with larger rudder and the elevator of the SZD-42-2 Jantar 2. The design life is 15,000 hours, though at present it is approved for only 4,000 hours

panoramic camera and carrying eight film return capsules, Orlets-1 had a design life of 60 days. After completing its mission, the satellite was detonated

intended to replace the CR4000s, which are reaching the end of their design life. TfL Bus & Tram Passes are valid on Tramlink, as are Travelcards that

possibly resulting in the tunnel not lasting for the proposed 100-year design life. Further tunnel leaks were also discovered in 2007, but were unrelated

mechanical. By 1974, the T2 had gained its final shape. Very late in the T2's design life, during the late 1970s, the first prototypes of Type 2 vans with four-wheel

1,364 kg (3,007 lb) after reaching geostationary orbit and an 8-year design life. When stowed for launch, its dimensions were 3.4 m (11 ft) long and 3

and rate of precession.: 423  OV3-1 massed 77 kilograms (170 lb) Its design life-span was one year.: 423 : 422–423  OV3-4's scientific payload, provided

rate, and rate of precession.: 423  OV3-2 massed 81 kg (179 lb) Its design life-span was one year.: 423  OV3-2 carried five AFCRL experiments designed

from the roof using massive steel beams [clarification needed]. The design life of 120 years meant that aluminium bronze was chosen for exposed metal

to 2001, 2012 to 2013, and 2015 into the present. Originally given a design life of 35 years, both Quebec's use of de-icing salt for its roadway infrastructure

land mobile service, and television and radio programming. Each had a design life of 7 years and a bandwidth of 72 MHz. ECS-3 was lost in an Ariane 3 launch

The S family has received various upgrades and enhancements over its design life. A 5-Speed Manual Transmission. Ratios: First Gear: 3.538:1 Second Gear:

(669 ft), 6×342 m (1,122 ft), 204 m (669 ft) Clearance below 270 m (890 ft) Design life 120 years History Designer Dr Michel Virlogeux, structural engineer Constructed

for shield contact and mechanical retention. The eSATA connector has a design-life of 5,000 matings; the ordinary SATA connector is only specified for 50

designed with a life expectancy of 15 years, significantly longer than the design life of Globalstar's first-generation constellation. The second- generation

power in 2007, and concluded operations after just over half of its design life 31 March 22:09 Delta II 7925-9.5 Cape Canaveral SLC-17A Boeing IDS GPS

Applications Crewed spaceplane Specifications Launch mass 19.950 kg Regime Low Earth Design life 1979 to 1982 Production Status Cancelled (1982) Launched 0

network. The satellite lasted 10 years and 6.5 months, short of the design life of 12 years. Spaceflight portal Yamal-202 – Satellite that was launched

Future Group. In March 2019, he opened a learning centre for art and design, life skills, performing arts and vedic science and ethics in Hyderabad. The

ca/eng/satellites/cassiope.asp Mission duration Primary mission: 18 months Design life: 2 years Elapsed: 10 years, 8 months, 4 days Orbits completed 53807 Spacecraft

examples over 50 metres (160 ft) Width examples over 1.5 metres (5 ft) Design life up to 500 years History Architect War Khasis, War Jaintias, Konyak Nagas

original satellites based on the LM-700A model had been projected to have a design life of only 8 years. The second-generation Iridium-NEXT satellites began

different fields and industries, which include weather forecast, drug design, life science, auto design, new material, civil engineering, physics, chemistry

A2100M Launch mass 6,168 kg (13,598 lb) Regime Geosynchronous orbit Design life 14 years (planned) Production Status Operational Active On order 0 Built

the satellite with a small X-band ground station. The satellites had a design life of 12 years, with an orbital maneuver life of 15 years, which means that

which is a service lifespan of over 50 years and well in excess of the design life of 25–30 years for the average diesel locomotive. Furthermore, when life-expired

set to be a closed nuclear fuel cycle. AHWR-300 is expected to have design life close to 100 years and will utilise Uranium-233 produced in the fast-breeder

04382 and International Designator 1970-034A. Dong Fang Hong 1 had a design life of 20 days. During that time, it transmitted telemetry data and space

2011. It stopped collecting data on 11 December 2010, after 13 years (design life was 5 years). It had a mass of 309 kg and was built by Orbital Sciences

successfully, the agency lost its control within two years despite the design life of five years with no investigations that were conducted. Between 1993–94

One power output will be 1170 MWe gross, 1090 MWe net, with a 60-year design life, and would use a combination of passive and active safety systems with

Longest span 240 m (787.40 ft) Clearance below 38.5 metres (126 ft) Design life 125 years History Architect Poul Ove Jensen Designer T.Y. Lin International

operations team to safely operate the mission well past its intended design life. JPL · 128604 128607 Richhund 2004 QJ18 Rich Hund (born 1956) is the

has identified 224 bridges along Acela's route that are beyond their design life. To prepare for the Acela launch, Amtrak upgraded the track along the

one-way) Crew capacity 4 Regime Near-rectilinear halo orbit Lunar landing Design life 30 days Dimensions Height 16 m (52 ft) Production Status In development

transponders (NATO B / D band) Data rate of up to 64 kbit/s) Regime Low Earth Design life 5 years Production Status Operational Retired Yes Related spacecraft

Page McConnell – keyboards, backing vocals, lead vocals on "Strange Design", "Life on Mars?", "It's Ice" and "A Day in the Life", acapella vocals on "Hello

signed an order to do so. By this stage Mir was well past the end of its design life, and Rosaviakosmos General Director Yuri Koptev believed that "any of

Taylor & Francis. ISBN 978-0-240-80984-7. "Printer Ink Cartridges". Design Life-Cycle. Retrieved 2020-08-06. Bouton (2008-01-01). Coreldraw X4: Official

orbit most of the satellites re-entered before reaching their intended design life. TechEdSat-9 and TechEdSat-11 are planned to fly at some point in the

IRS-1D, but also to enhance the data quality. Although IRS-P6 had a design life of five years, the satellite was still operational as of October 2015

2012 that the GTP had been in operation for seven years of its 30-year design life cycle. The Botany chemical plant released mercury vapour into the atmosphere

Astra 23.5°E to replace Astra 1D, which was approaching the end of its design life. Following the launch of Astra 1M to the Astra 19.2°E position in November

projects have been exhibited in the Cooper-Hewitt National Design Museum’s “Design Life Now: National Design Triennial 2006” and at the Guggenheim Museum. A

2 Mbit/s (typical, average) Primary mission duration: 10 to 18 years Design life: 3 years. Magnetic field intensity: 0.15 tesla produced by a 1,200 kg

year after schedule. The new bridges were designed to have a 120-year design life. The causeway consists of two bridges and a causeway, with a total length

Simon & Schuster. Retrieved 12 January 2023. "WATCH Sarah Richardson Design Life". Sarah Richardson Design. "Sarah Richardson". YouTube. Retrieved 12

Applications Communications Specifications Power 16 kW Regime Geostationary Design life 15 years Production Status In production On order 7 Built 74 Launched

No. of spans 1 Clearance below 9 m (30 ft) from mean high water level Design life 120 years History Architect Arenas & Asociados Construction end 5 October

involves the common stages of development. For example, a generic software design life cycles has following steps: Communication. Planning. Modeling which involves

situated in the South West of Ireland, a station which will approach its design life in 2025 and until then it will remain as Ireland's primary emitter of

(minimum) Traction, electric 750 V DC overhead Right-of-way width, 9–15 m Design life, 60 years Speed, 80 km/h (maximum) Train set length, 30 m Inter-station

transponders, as well as 18 "reverse-band" transponders. The satellite has a design life of 15 years and is located at 99° W. T15 (formerly DirecTV 15) was successfully

current New Zealand building code requires a building with a 50-year design life to withstand predicted loads of a 500-year event. Initial reports by

in Queensland's history. The duplicate bridge was specified to have a design life of 300 years. To the south, the upgrade included widening 12 km (7 mi)

before completing the fourth, which was overseen by another artist to his design. Life-sized plaster maquette (at Canterbury Heritage Museum as of 2013) and

October 2012. Eutelsat 8 West B is a 5,782 kg (12,747 lb) satellite with a design life of 15 years. It is equipped with an S400-12 apogee motor which was used

Operator Roskosmos Applications Crewed spaceplane Specifications Regime Low Earth Design life 2004 to 2006 Production Status Cancelled (2006) Launched 0

customers. The Cartosat-2D weighs 714 kilograms (1,574 lb), and its design life is five years. The two Indian nanosatellites, designated INS-1A and INS-1B

satellite lasted 4079 days (11 years and 2 months), a bit short of the design life of 12.5 years. Yamal-300K was launched along Luch 5B 2 November 2012

Believe It Or Not and Guinness World Records in April 1999). TDRS-1 had a design life of ten years, however in April 2008, it was still operational on the

in which buildings and other structures were housed. The camp had a design life span of 10 years with appropriate maintenance. It was permanently manned

commission the system was completed in seven months, and the system has a design life of 25 years. The Osmanabad region in Maharashtra has abundant sunlight

Arches: Seven Piers in water Five Clearance below 31 metres (102 ft) Design life 1893: wooden deck replaced in steel 1938/40: iron chains replaced in

(1.49 to 1.65 tons) after reaching geostationary orbit, and an 8-year design life. When stowed for launch, its dimensions were 3.4 m (11 ft) in height

modifications during construction are either unfeasible or very expensive. The design life of these structures often ranges between 25–50 years. The environmental

to businesses with a 5-meter antenna. It has reached the end of its design life expectancy. SkyTerra-1 was launched in mid-November 2010, providing North

(Robin Joseph and Kim Leow) In a Heartbeat (Ringling College of Art and Design) Life Smartphone (Central Academy of Fine Arts) Lost Property Office (Daniel

elements, it required a speed of 110 km/h for fully laden trains, a minimum design life of 35 years and the ability to climb the steep grades of the proposed

can should have a fender spacing of about 25–50% of the ship's length. Design life of port fenders will vary by ship type, berthing frequency, temperature

current per contact (pole), maximum fault withstand current, duty cycle, design life expectancy, voltage, and coil voltage. A general purpose motor control

Applications Technology demonstration Specifications Regime Low Earth (planned) Design life 2-4 months Production Status Failed Built 3 Launched 2 Lost 2 Maiden

Height: 3.58 m (11.7 ft) Volume 8 m3 (280 cu ft) Power Photovoltaic array Regime Low Earth orbit Design life 7 days Production Status In development

2000 and later sold on to United Utilities in 2001. The plant has a design life of twenty years. At the maximum consented flow rate, 60 m3/s of water

platform. It had a launch mass of 2,489 kg (5,487 lb) and a 10-year design life. When stowed for launch, its dimensions were 2.41 m × 2.58 m × 2.20 m

iron (original) sandstone ashlar steel (modern upgrade) No. of spans 1 Design life 1871: bridge deck replaced 1902: additional cables added 1974: bridge

replacement. During the late 1990s Mark 1 stock began to reach the end of its design life and concerns about its safety relative to newer rolling stock became

began to dismantle the turbine as it had reached near the end of its design life. Demolition was completed by November 8. The Pickering Wind Generating

900 kg (4,200 lb) Payload capacity 100 kg (220 lb) Power 200 W (0.27 hp) Design life 14 days after landing Dimensions Length 3 m (9.8 ft) Diameter 2 m (6 ft

needed] By 2007, the bridges were considered to be at the end of their design life, and a project to replace the bridges was begun. The first of the two

observatory used to study the cosmos. It was launched June 11, 2008, has a design life of 5 years and a goal of 10 years. The primary instrument is the Large

establish the Astra 23.5°E position) was approaching the end of its design life and was replaced at 23.5° east by Astra 1E. Astra 1D was moved to 31

the pressure tubes in the Pickering A reactors were replaced ahead of design life due to unexpected deterioration caused by hydrogen embrittlement. Extensive

and Communications (now Boeing Satellite Development Center) with a design life of 15 years providing direct-to-home digital TV distribution from the

particular concern over the ongoing use of Pacers beyond their intended design life." Northern Rail insisted that the trains were safe, and that they are

have to be closed by 2015 under these plans, with around 10 years of design life still remaining. It was also noted that, apart from being difficult to

original on 2 November 2019. Retrieved 2 November 2019. They have a 35-year design life. Syal, Rajeev; Topham, Gwyn (2 January 2020). "Troubled rail firm Northern

surgeon. Dr. Myo Thant, The Surgeon's designer, would later go on to design Life & Death, a surgical game with similar elements, albeit with a wider release

experimental aircraft, the engines are often run to their complete 2250-hour design life before overhaul[citation needed]. The M14-V26 variant has been developed

463 ft (141 m) Width 42 ft (13 m) Clearance below 46 ft (14 m) (low tide) Design life 1899: cast iron piers are added to reduce the load on the tubes and permit

wider at 3.0 meters) is 2.6 meters. It is a VVVF AC drive and has a design life of 30 years. 05C01 stocks has 4 carriages with 172 seats which could

Best Actor, Best Original Song, Best Production Design, Best Costume Design) Life of Pi (Best Picture, Best Adapted Screenplay, Best Original Song, Best

length 2,235 feet (681 m) Longest span 700 feet (210 m) Piers in water 2 Design life 39 years (until collapse) History Designer J. E. Greiner Company Constructed

likely to be limited to small-scale habitats and orbital modules with design life cycles of only several years or decades.[citation needed] The designs