![]() Vostok-2M rocket | |
Function | Carrier rocket |
---|---|
Manufacturer | OKB-1 |
Country of origin | USSR |
Size | |
Stages | Two |
Capacity | |
Payload toSSO | |
Mass | 3,800 kilograms (8,400 lb) |
Associated rockets | |
Family | R-7 |
Launch history | |
Status | Retired |
Launch sites | Baikonur,Site 31/6 Plesetsk, Sites41/1,16/2,43/3 &43/4 |
Total launches | 93 |
Success(es) | 92 |
Failure(s) | 1 |
First flight | 28 August 1964 |
Last flight | 29 August 1991 |
Carries passengers or cargo | Meteor Resurs Tselina-D |
Boosters | |
No. boosters | 4 |
Powered by | 1RD-107-8D74K |
Maximum thrust | 995.3 kilonewtons (223,800 lbf) |
Burn time | 120 seconds |
Propellant | RP-1/LOX |
First stage | |
Powered by | 1RD-108-8D75K |
Maximum thrust | 940.4 kilonewtons (211,400 lbf) |
Burn time | 305 seconds |
Propellant | RP-1/LOX |
Second stage | |
Powered by | 1RD-0109 |
Maximum thrust | 54.52 kilonewtons (12,260 lbf) |
Burn time | 400 seconds |
Propellant | RP-1/LOX |
TheVostok-2M (Russian:Восток,lit. 'East'),GRAU index:8A92M was anexpendablecarrier rocket used by theSoviet Union between 1964 and 1991. Ninety-three were launched, of which one failed.[1] Another was destroyed before launch.[2] It was originally built as a specialised version of the earlierVostok-2, for injecting lighter payloads into higherSun-synchronous orbits. It was a member of theR-7 family of rockets, and the lastVostok.
The Vostok-2M was similar to the Vostok-2 booster but the adapter portion of the Blok E stage remained attached to the payload and the guidance system was modified specially to assist in putting payloads in sun-synchronous orbits. Vehicles flown in 1967 and later used the 8D74M engines or the 11D511 in 1973 and later.
The Vostok-2M made its maiden flight on 28 August 1964 fromSite 31/6 at theBaikonur Cosmodrome, successfully placingKosmos 44, aMeteorweather satellite into orbit. A total of 93 were launched from 1964 to '91. Its only launch failure occurred on 1 February 1969, when the launch of a Meteor failed due to anupper stage problem.
At 16:01 GMT on 18 March 1980,a Vostok-2M exploded during fueling atPlesetskSite 43/4, ahead of the launch of aTselina-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 contacthydrogen peroxide.[3] 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, andSites 41/1, 16/2, 43/3 and 43/4 at Plesetsk.[1] The Vostok-2M was retired in 1991 in favour of standardization on theSoyuz-U andU2 rockets. The final flight was conducted on 29 August and carried theIRS-1B satellite for theIndian Space Research Organization.