Dnepr (rocket)
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Function | Orbital carrier rocket |
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Manufacturer | Yuzhny Machine-Building Plant |
Country of origin | Soviet Union (Ukraine) |
Size | |
Height | 34.3 metres (113 ft) |
Diameter | 3 metres (9.8 ft) |
Mass | 211,000 kilograms (465,000 lb) |
Stages | 3 (4 or 5 with SpaceTug upper stages) |
Capacity | |
Payload to LEO | |
Mass | 4,500 kilograms (9,900 lb) |
Payload to the ISS | |
Mass | 3,200 kilograms (7,100 lb) |
Payload to TLI | |
Mass | 550 kilograms (1,210 lb) (with ST-1) |
Associated rockets | |
Based on |
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Launch history | |
Status | Active |
Launch sites | LC-109, Baikonur Yasny |
Total launches | 13 |
Success(es) | 12 |
Failure(s) | 1 |
First flight | 21 April 1999 |
Powered by | 1 RD-264 |
Maximum thrust | 4,520 kilonewtons (1,020,000 lbf) |
Specific impulse | 318 s |
Burn time | 130 seconds |
Propellant | N2O4/UDMH |
Powered by | 1 RD-0255 |
Maximum thrust | 755 kilonewtons (170,000 lbf) |
Specific impulse | 340 sec |
Burn time | 190 seconds |
Propellant | N2O4/UDMH |
Powered by | 1 RD-869 |
Maximum thrust | 18.6 kilonewtons (4,200 lbf) |
Specific impulse | 317 sec |
Burn time | 1,000 seconds |
Propellant | N2O4/UDMH |
SpaceTug 1 | |
Powered by | 1 Solid |
Propellant | Solid |
SpaceTug 3 | |
Powered by | 1 Liquid |
Propellant | N2O4/UDMH |
The Dnepr rocket ([Дніпро, Dnipro] Error: {{Lang-xx}}: text has italic markup (help); [Днепр, Dnepr] Error: {{Lang-xx}}: text has italic markup (help)) is a space launch vehicle named after the Dnieper River. It is a converted ICBM used for launching artificial satellites into orbit, operated by launch service provider ISC Kosmotras. The first launch, on April 21, 1999, successfully placed UoSAT-12, a 350 kg demonstration mini-satellite, into a 650 km circular LEO.[1][2]
Converted missile
The Dnepr is based on the R-36MUTTH ICBM– called the SS-18 Satan by NATO– designed by the Yuzhnoe Design Bureau in Dnipropetrovsk, Ukraine. The Dnepr is three-stage rocket using storable hypergolic liquid propellants. The launch vehicles used for satellite launches are withdrawn from service with the Russian Strategic Rocket Forces and stored for commercial use. A group of 150 ICBMs can be converted for use and are available until 2020. The Dnepr can be launched from Baikonur in Kazakhstan and a newly created Cosmodrome at the Dombarovsky launch base, near Yasny, in the Orenburg region of Russia.
Performance
The Dnepr launch vehicle has only a small number of modifications compared to the R-36M ICBM in service. The main difference is the payload adapter located in the space head module and modified flight-control unit. This baseline version can lift 3,600 kg into a 300 km low earth orbit at an inclination of 50.6°, or 2,300 kg to a 300 km sun-synchronous orbit at an inclination of 98.0°. On a typical mission the Dnepr deploys a larger main payload and a secondary payload of Miniaturized satellites and CubeSats. A number of Space Tugs are under development which will be placed inside the space head module, thereby sacrificing volume and payload but enabling orbits requiring more energy, including planetary escape orbits.
Launch history
Before the Dnepr entered commercial service it was in service with the Strategic Rocket Forces which launched the ICBM version over 160 times with a reliability of 97%. The rocket has been used twelve times for commercial purposes with a single failure.
Flight | Date | Payload | Orbit | Site |
---|---|---|---|---|
1 | April 21, 1999 | UoSAT-12 | 650 km circular LEO at 65˚ inclination | Baikonur |
2 | September 26, 2000 | MegSat-1 (Italy)/UniSat (Italy)/TiungSat-1 (Malaysia)/ SaudiSat-1A & SaudiSat 1B (Saudi Arabia) | 650 km circular LEO at 65˚ inclination | Baikonur |
3 | December 20, 2002 | LatinSat 1 & LatinSat 2 (Argentina)/SaudiSat-1S (Saudi Arabia)/UniSat 2 (Italy)/Rubin 2 (Germany) | 650 km circular LEO at 65˚ inclination | Baikonur |
4 | June 29, 2004 | Demeter (France)/ Saudicomsat-1, Saudicomsat 2 & Saudisat 2 (Saudi Arabia)/ LatinSat C & LatinSat D (Argentina)/ Unisat-3 (Italy)/ Amsat Echo (USA) | 700 km × 850 km Sun-synchronic orbit at 98˚ inclination | Baikonur |
5 | August 24, 2005 | OICETS & INDEX (Japan) | 600 km × 50 km Sun-synchronic orbit at 98˚ inclination | Baikonur |
6 | July 12, 2006 | Genesis I (USA) | 560 km circular LEO at 65˚ inclination | Yasny |
7 | July 26, 2006 | BelKA (Belarus)/ UniSat-4 & PiCPoT (Italy)/ Baumanets ( Russia)/ AeroCube-1, CP1, CP2, ICEcube-1, ICEcube-2, ION, KUTESat, Merope, Rincon 1, Mea Huaka`i (Voyager) & SACRED (USA)/HAUSAT-1 (South Korea)/Ncube-1 (Norway)/SEEDS (Japan) | failed to reach orbit | Baikonur |
8 | 17 April, 2007 | EgyptSat 1/SaudiSat 3/SaudiComSat 3-7 /AKS 1/AKS 2/Cal Poly Picosatellite Project 3 &4/CAPE 1/Libertad 1/AeroCube 2/CubeSat TestBed 1/MAST | 692 km × 665 km Sun synchronous orbit at 98˚ inclination[3] | Baikonur |
9 | 15 June, 2007 | TerraSAR-X | 514 km circular LEO at 97˚ inclination[4] | Baikonur |
10 | 28 June, 2007 | Genesis II | 560 km circular LEO at 65˚ inclination | Yasny |
11 | 2008-08-29 | RapidEye 1/2/3/4/5 | [5] | Baikonur |
12 | 1 October 2008 | THEOS | SSO | Yasny |
13 | July 29, 2009 | DubaiSat-1/Deimos-1/UK-DMC 2/Nanosat 1B/AprizeSat-3/AprizeSat-4 | SSO | Baikonur |
14 | July, 2009 | [Cluster launch] | planned | Yasny |
15 | October, 2009 | Tandem-X | planned | Baikonur |
16 | November, 2009 | [Cryosat-2] | planned | Baikonur |
17 | March, 2010 | [Sitch 2 cluster launch] | planned | Yasny |
Launch failure
The committee investigating the failed launch on July 26, 2006 concluded that the failure was caused by a malfunctioning of the pumping hydraulic drive of combustion chamber #4. The control malfunctioning brought about the disturbances, which led to the roll instability, excessive dispersions of the yaw and pitch angles. Thrust termination occurred at 74 seconds after lift off. The crash site was located 150 km from the launch pad in an unpopulated area of Kazakhstan. Toxic propellants did pollute the crash site, forcing Russia to pay US$1.1m in compensation[6]. The rocket used for this launch was more than twenty years old. Procedures for launch have been changed to prevent future malfunctions of this kind.
References
- ^ "The Dnepr launcher". RussianSpaceWeb.com.
- ^ "UoSAT-12 Integrates with Dnepr for Launch on 21 April". Surrey Satellite Technology Ltd.
- ^ "EgyptSat 1/Saudisat-3 launch details" (in Russian). Roskosmos.
- ^ "TerraSAR-X launch details" (in Russian). Roskosmos.
- ^ "Five RapidEye remote sensing satellites launched". Spaceflight Now.
- ^ "Russia to pay Kazakhstan over US$1 million in compensation for damage from rocket crash". International Herald Tribune. 2006-10-03.
External links
- "Kosmotras launch service provider".
- "DNEPR User's guide" (PDF). MIT. November 2001.
{{cite web}}
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(help) - "Astronautix entry - R-36M2".
- "Space Calendar (JPL)". NASA.