 Drawing of the Kosmos-3M with bulges onpayload fairing for launchingSAR Lupe | |
| Function | Orbitallaunch vehicle |
|---|---|
| Manufacturer | Yuzhnoye /NPO Polyot |
| Country of origin | Soviet Union, Russia |
| Size | |
| Height | 32.4 m (106 ft) |
| Diameter | 2.4 m (7 ft 10 in) |
| Mass | 109,000 kg (240,000 lb) |
| Stages | 2 |
| Capacity | |
| Payload toLow Earth orbit | |
| Mass | 1,500 kg (3,300 lb) |
| Payload toSun-synchronous orbit | |
| Mass | 775 kg (1,709 lb) |
| Launch history | |
| Status | Retired |
| Launch sites | Plesetsk Cosmodrome, Site 132 Site 133/3 Kapustin Yar Site 107 |
| Total launches | 444 |
| Success(es) | 424 |
| Failure(s) | 20 |
| First flight | 15 May 1967 |
| Last flight | 27 April 2010 |
| First stage – R-14U | |
| Powered by | 1RD-216 |
| Maximum thrust | 1,485 kN (334,000 lbf) |
| Specific impulse | 291 seconds |
| Burn time | 131 seconds |
| Propellant | AK27I /UDMH |
| Second stage – S3M | |
| Powered by | 111D49[1] |
| Maximum thrust | 157 kN (35,000 lbf) |
| Specific impulse | 293 seconds |
| Burn time | 350 + 350 seconds |
| Propellant | AK27I/UDMH |
TheKosmos-3M (Russian:Космос-3М meaning "Cosmos",GRAU index11K65M) was a Russian spacelaunch vehicle, member of theKosmos rocket family. It was a liquid-fueled two-stage launch vehicle, first launched in 1967 and with over 420 successful launches to its name.
The Kosmos-3M usedUDMH fuel andAK27I oxidizer (red fuming nitric acid) to lift roughly 1,400 kg (3,100 lb) of payload into orbit. It differed from the earlier Kosmos-3 in its finer control of the second-stage burn, allowing operators to tune the thrust and even channel it through nozzles that helped orient the rocket for the launching of multiple satellites at one time.
PO Polyot manufactured these launch vehicles in the Russian city ofOmsk for decades. It was originally scheduled to be retired from service in 2011;[2] however, in April 2010 the Commander of the Russian Space Forces confirmed that it would be retired by the end of 2010.[3] One further launch, withKanopus-ST, was planned; however, this was cancelled in late 2012 as the launch vehicle had exceeded its design life while in storage ahead of the launch.
 |
| Date | Site | Payload(s) | References |
|---|---|---|---|
| 19 April 1975 | Kapustin Yar | Aryabhata | |
| 7 June 1979 | Kapustin Yar | Bhaskara I | [4] |
| 20 November 1981 | Kapustin Yar | Bhaskara II | [5] |
| 28 April 1999 | Kapustin Yar | ABRIXAS | [6] |
| 28 June 2000 | Plesetsk | Nadezhda, Tsinghua-1,SNAP-1 | [7][8] |
| 28 Nov 2002 | Plesetsk | ALSAT-1, Mozhayets | [9][10] |
| 27 Sept 2003 | Plesetsk | NigeriaSAT-1,BILSAT-1,UK-DMC (BNSCSat), Mozhayets-4,KAISTSat-4, Larets, Rubin-4 | [10][11] |
| 2 July 2007 | Plesetsk | SAR-Lupe-2 | |
| 11 September 2007 | Plesetsk | Kosmos-2429 | |
| 27 March 2008 | Plesetsk | SAR-Lupe 4 | |
| 19 June 2008 | Kapustin Yar | Orbcomm | [citation needed] |
| 22 July 2008 | Plesetsk | SAR-Lupe 5 | |
| 21 July 2009 | Plesetsk Site 132/1 | Kosmos 2454 (Parus) Sterkh-1 |
A total of 446 Kosmos 3Ms were launched from 1967 to 2010, with 22 failures. Some of the more noteworthy ones:
On 22 December 1970, a launch of a target vehicle for ASAT tests lost thrust at liftoff and fell back onto the pad at Plesetsk, exploding and badly damaging it.[citation needed]
On 26 June 1973, a Kosmos 3M exploded on the pad at Plesetsk during a propellant loading accident, killing nine people.[12]
An attempted launch of an Intercosmos scientific satellite on 3 June 1975 failed 84 seconds into the launch when the first stage engine shut down.[citation needed]
An attempted launch of a military radar calibration satellite on 25 January 1983 suffered another first stage failure about 40 seconds into launch when the RD-219 started losing thrust. The onboard computer automatically shut the engine off and the launch vehicle fell into theNorthern Dvina. Due to the tense relations between the U.S. and Soviet Union at this time, the U.S. military was widely suspected of having shot down the launch vehicle and General SecretaryYuri Andropov personally informed of this possibility. However, a group of locals ice fishing in the Dvina had witnessed the booster plunge into the river and reported what they'd seen to authorities. After this and a quick examination of telemetry, sabotage was ruled out. The failure was traced to high-frequency combustion instability, which had been a problem with the RD-219 engine and was also responsible for the 1970 and 1975 Kosmos 3M failures. The engine was redesigned and no further launches were lost due to first stage engine failures.[citation needed]
More recently, on 21 November 2000, a Kosmos 3M launcher failed to place theQuickBird 1 satellite into orbit due to a failure of its second stage. The launch vehicle and satellite reentered the atmosphere overUruguay, and an inquest into the accident was inconclusive.[citation needed]