Dnepr (rocket)


The Dnepr rocket was a space launch vehicle named after the Dnieper River. It was 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 Low Earth orbit.

History

The Dnepr was based on the R-36MUTTH Intercontinental ballistic missile called the SS-18 Satan by NATOdesigned in the 1970s by the Yuzhnoe Design Bureau in Dnipro, Ukraine, which was then a part of the USSR.
The Dnepr control system was developed and produced by the JSC "Khartron", Kharkiv. The Dnepr was a three-stage rocket using storable hypergolic liquid propellants. The launch vehicles used for satellite launches have been withdrawn from ballistic missile service with the Russian Strategic Rocket Forces and stored for commercial use. A group of a total of 150 ICBMs were allowed under certain geopolitical disarmament protocols to be converted for use, and can be launched through 2020. The Dnepr was launched from the Russian-controlled Baikonur cosmodrome in Kazakhstan and the Dombarovsky launch base, near Yasny, in the Orenburg region of Russia.
In February 2015, following a year of strained relations as a result of a Russian military intervention into Ukraine, Russia announced that it would sever its "joint program with Ukraine to launch Dnepr rockets and no longer interested in buying Ukrainian Zenit boosters, deepening problems for space program and its struggling Yuzhmash factory." However ISC Kosmotras reported that they would continue to fulfill its obligations for three Dnepr launches in 2015, of which only one took place.
By the end of 2016, no further launch had materialized and the remaining customers had switched to alternative launch providers.

Performance

The Dnepr launch vehicle had only a small number of modifications compared to the R-36M ICBM in service. The main difference was the payload adapter located in the space head module and modified flight-control unit. This baseline version could 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 deployed a larger main payload and a secondary payload of Miniaturized satellites and CubeSats.

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 had been used several times for commercial purposes with a single failure.
The Dnepr has at two points held the record for the most satellites orbited in a single launch; the April 2007 launch with 14 payloads held the record until 20 November 2013, when an American Minotaur I placed 29 satellites and two experiment packages into orbit. The next day a Dnepr re-took the record, placing 32 satellites and an experiment package bolted to the upper stage into low Earth orbit. This record was broken by an Antares launch in January 2014 which carried 34 spacecraft.
FlightDate PayloadOrbitSite
1April 21, 1999
04:59
UoSAT-12LEO 650 km / 65˚Baikonur
2
10:05
LEO 650 km / 65˚Baikonur
3December 20, 2002
17:00
LEO 650 km / 65˚Baikonur
4June 29, 2004
06:30
SSO 700 × 850 km / 98˚Baikonur
5August 23, 2005
21:10
SSO 600 × 550 km / 98˚Baikonur
6July 12, 2006
14:53
Genesis I LEO 560 km / 65˚Yasny
7July 26, 2006
19:43
failed to reach orbitBaikonur
8April 17, 2007
06:46
Baikonur
9June 15, 2007
02:14
TerraSAR-XLEO 514 km / 97˚Baikonur
10June 28, 2007
15:02
Genesis IILEO 560 km / 65˚Yasny
11August 29, 2008
07:16
RapidEye 1-5Baikonur
12October 1, 2008
06:37
THEOSSSOYasny
13July 29, 2009
18:46
SSOBaikonur
14April 8, 2010
13:57
Cryosat-2PolarBaikonur
15June 15, 2010
14:42
SSOYasny
16June 21, 2010
02:14
TanDEM-XLEOBaikonur
17August 17, 2011
07:12
LEOYasny
18August 22, 2013
14:39
KOMPSat-5LEOYasny
19November 21, 2013
07:10
LEOYasny
20June 19, 2014
19:11
LEOYasny
21November 6, 2014
07:35
LEOYasny
22March 25, 2015
22:08
KOMPSat-3ALEOYasny

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 polluted the crash site, forcing Russia to pay US$1.1m in compensation. 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.