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Salyut 2

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Failed Soviet space station (1973)

Salyut 2 (OPS-1)
Station statistics
COSPAR ID1973-017A
SATCATno.06398Edit this on Wikidata
Call signSalyut 2
Crew3
Launch3 April 1973
09:00:00 UTC
Launch padBaikonurSite 81/23[1]
Reentry28 May 1973
Mass18,500 kilograms (40,800 lb)
Length14.55 metres (47.7 ft)
Diameter4.15 metres (13.6 ft)
Pressurisedvolume99 cubic metres (3,500 cu ft)
Periapsis altitude257 kilometres (160 mi)
Apoapsis altitude278 kilometres (173 mi)
Orbital inclination51.6°
Orbital period89.8 minutes
Days in orbit54 days
No. of orbits866
Distance travelled35,163,530 kilometres (21,849,600 mi)
Statistics as of 4 April 1973
Configuration
An Almaz space station

Salyut 2 (OPS-1) (Russian:Салют-2 meaningSalute 2) was aSovietspace station which was launched in 1973 as part of theSalyut programme. It was the firstAlmaz military space station to fly. Within two weeks of its launch, the station had lost altitude control and depressurized, leaving it unusable. Its orbit decayed and it re-entered the atmosphere on 28 May 1973, without any crews having visited it.

Spacecraft

[edit]
Main article:Almaz

Salyut 2 was an Almaz military space station.[2] It was designated part of the Salyut programme in order to conceal the existence of the two separate space station programmes.[3]

Salyut 2 was 14.55 metres (47.7 ft) long with a diameter of 4.15 metres (13.6 ft),[4][5][6] and had an internal habitable volume of 90 cubic metres (3,200 cu ft). At launch it had a mass of 18,950 kilograms (41,780 lb).[7] A single aft-mounted docking port was intended for use bySoyuz spacecraft carrying cosmonauts to work aboard the station. Twosolar arrays mounted at the aft end of the station near the docking port provided power to the station, generating a total of 3,120 watts of electricity.[8] The station was equipped with 32 attitude control thrusters, as well as twoRD-0225 engines, each capable of generating 3.9 kilonewtons (880 lbf) of thrust, for orbital manoeuvres.[7]

Launch

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Salyut 2 was launched fromSite 81/23 at theBaikonur Cosmodrome, atop a three-stageProton-K rocket, serial number 283-01.[9] The launch took place at 09:00:00 UTC on 3 April 1973,[10] and successfully placed Salyut 2 intolow Earth orbit.[9] Upon reaching orbit, Salyut 2 was assigned theInternational Designator 1973-017A, whilstNORAD gave it theSatellite Catalog Number 06398.[1] The third stage (8S812) of the Proton-K rocket entered orbit along with Salyut 2. On 4 April, it was catalogued in a 192 by 238 kilometres (119 by 148 mi) orbit, inclined at 51.4 degrees.[11]

Failure

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Three days after the launch of Salyut 2, the Proton's spent third stage exploded, due to pressure changes within the tanks. This explosion resulted in a cloud of debris, some of which followed a similar trajectory to the station. Ten days later this debris struck the station, damaging the hull and causing depressurization. Both solar panels were torn free, removing the ability of the station to generate power and control its attitude.[3][1]

Three pieces of debris from the station were catalogued, and haddecayed from orbit by 13 May.[11] The remainder of the stationreentered the atmosphere on 28 May 1973[2][11] over thePacific Ocean.[4]

An inquiry into the failure initially determined that a fuel line had burst, burning a hole in the station.[3] The damage from the debris collision was only discovered later.[when?]

Fidel Castro tour

[edit]

When First Secretary of the Communist Party ofCubaFidel Castro was in theSoviet Union as part of a whirlwind tour in 1972, General Secretary of the Communist Party of theSoviet UnionLeonid Brezhnev broughtFidel Castro to theGagarin Cosmonaut Training Centre.[12] Fidel Castro was photographed inside both theSoyuz docking trainer[13][better source needed] and the Salyut-2 (OPS-1/Almaz) military space station.[14][better source needed]

See also

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References

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  1. ^abc"Salyut 2". United States National Space Data Center. 8 October 2010. Retrieved4 January 2010.
  2. ^abPortree, David S. F. (March 1995)."Mir Hardware Heritage"(PDF). NASA. Archived fromthe original(PDF) on 7 September 2009. Retrieved4 January 2011.
  3. ^abcZak, Anatoly."OPS-1 (Salyut-2) space station".RussianSpaceWeb. Retrieved4 January 2011.
  4. ^abMark Wade."Almaz OPS | Part of Almaz Family".Encyclopedia Astronautica. Archived fromthe original on 20 August 2016.
  5. ^Emied Jacinto (6 May 2013)."Space Station".Mousehunt – viaSlideShare.
  6. ^David M. Harland."Salyut | Soviet Space Station Series".Encyclopædia Britannica.
  7. ^abZak, Anatoly."Almaz space station technical overview".RussianSpaceWeb. Retrieved5 January 2011.
  8. ^Zak, Anatoly."Almaz space station technical overview - Transfer section".RussianSpaceWeb. Retrieved5 January 2011.
  9. ^abWade, Mark."Proton-K".Encyclopedia Astronautica. Archived fromthe original on 22 August 2010. Retrieved2 January 2011.1973 April 3...Launch Vehicle: Proton-K. LV Configuration: Proton-K 283-01...Salyut 2
  10. ^McDowell, Jonathan."Launch Log".Jonathan's Space Page. Retrieved4 January 2011.
  11. ^abcMcDowell, Jonathan."Satellite Catalog".Jonathan's Space Page. Retrieved4 January 2011.
  12. ^"Castro Speech Data Base - Latin American Network Information Center, LANIC".
  13. ^"REGION, USSR. First Secretary of the Communist Party of Cuba Fidel". Archived fromthe original on 11 May 2021.
  14. ^"Moscow. General Secretary of the Central Committee of the CPSU Leonid". Archived fromthe original on 12 May 2021.
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Notes: † Never inhabited due to launch or on-orbit failure, ‡ Part of theAlmaz military program, ° Never inhabited, lacks docking mechanism.
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated inunderline. Uncatalogued launch failures are listed initalics. Payloads deployed from other spacecraft are denoted in (brackets).

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