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From Wikipedia, the free encyclopedia

Vostok-2M
Vostok 8A92M.svg
Vostok-2M rocket
FunctionCarrier rocket
ManufacturerOKB-1
Country of originUSSR
Size
StagesTwo
Capacity
Payload to SSO
Mass3,800 kilograms (8,400 lb)
Associated rockets
FamilyR-7
Launch history
StatusRetired
Launch sitesBaikonur Site 31/6
Plesetsk Site 41/1 & 43
Total launches93
Success(es)92
Failure(s)1
First flight28 August 1964
Last flight29 August 1991
Notable payloadsMeteor
Resurs
Tselina-D
Boosters
No. boosters4
Engines1 RD-107-8D74K
Thrust995.3 kilonewtons (223,800 lbf)
Burn time120 seconds
FuelRP-1/LOX
First stage
Engines1 RD-108-8D75K
Thrust940.4 kilonewtons (211,400 lbf)
Burn time305 seconds
FuelRP-1/LOX
Second stage
Engines1 RD-0109
Thrust54.52 kilonewtons (12,260 lbf)
Burn time400 seconds
FuelRP-1/LOX

The Vostok-2M (Russian: Восток meaning "East"), GRAU index 8A92M was an expendable carrier rocket used by the Soviet Union between 1964 and 1991. Ninety-three were launched, of which one failed. Another was destroyed before launch.[1] It was originally built as a specialised version of the earlier Vostok-2, for injecting lighter payloads into higher sun-synchronous orbits. It was a member of the R-7 family of rockets, and the last Vostok.

The Vostok-2M made its maiden flight on 28 August 1964, from Site 31/6 at the Baikonur Cosmodrome, successfully placing Kosmos 44, a Meteor weather satellite into orbit. Its only launch failure occurred on 1 February 1969, when the launch of a Meteor failed due to an upper stage problem.

At 16:01 GMT on 18 March 1980, a Vostok-2M exploded during fueling at Plesetsk Site 43/4, ahead of the launch of a Tselina-D satellite, killing 48 people who were working on the rocket at the time. A filter in a hydrogen peroxide tank of the third stage had accidentally been soldered with lead instead of tin, with the catalytically active lead solder on the filter causing the explosion upon contact hydrogen peroxide.[2] As a consequence, the H2O2 broke down, overheated, and melted the solder, causing pieces to fall into the H2O2 storage tank and cause a runaway chemical reaction. This led to a fire inside the third stage and eventual explosion which resulted in the complete destruction of the launch vehicle and severe pad damage (LC-43 did not host another launch for three years).

Vostok-2M launches occurred from Site 31/6 at Baikonur, and Sites 41/1 and 43 at Plesetsk. It is unclear if any were launched from Site 1/5 at Baikonur. The Vostok-2M was retired in 1991, in favour of standardisation on the Soyuz-U and U2 rockets. The final flight was conducted on 29 August, and carried the IRS-1B satellite for the Indian Space Research Organisation.

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Transcription

References

  1. ^ Wade, Mark. "Vostok 8A92M". Encyclopedia Astronautica. Archived from the original on 2009-03-06. Retrieved 2009-04-15.
  2. ^ Boris Yevseyevich Chertok (2006-06-01). Rockets and People: Creating a rocket industry (PDF). Government Printing Office. pp. 636–640. ISBN 9780160766725.
This page was last edited on 5 January 2021, at 02:02
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