Strela
Khrunichev State Research and Production Space CenterRetired
Strela is a Russian orbital carrier rocket, derived from the Soviet/Russian UR-100NU missile. It conducted its maiden test launch on 5 December 2003, carried its first functional payload on 27 June 2013,and a second one on 19 December 2014.
Specifications
- Height
- 28.3 m
- Diameter
- 2.5 m
- Launch mass
- 105 t
- Stages
- 3
- LEO capacity
- 1,400 kg
Specifications from Launch Library. Figures the operator has not published are omitted.
Flight record
3flightswith a definitive outcome
100%success rate3 of 3
0failuresincluding partial failures
3success streakcurrent
First flight December 5, 2003 · latest December 19, 2014
Counted from padside's own launch record, the same basis as the stats page.
Flights per year
- Successful
- Failed
Show the numbers for Strela flights per year
| Year | Successful | Failed | Total |
|---|---|---|---|
| 2003 | 1 | 0 | 1 |
| 2004 | 0 | 0 | 0 |
| 2005 | 0 | 0 | 0 |
| 2006 | 0 | 0 | 0 |
| 2007 | 0 | 0 | 0 |
| 2008 | 0 | 0 | 0 |
| 2009 | 0 | 0 | 0 |
| 2010 | 0 | 0 | 0 |
| 2011 | 0 | 0 | 0 |
| 2012 | 0 | 0 | 0 |
| 2013 | 1 | 0 | 1 |
| 2014 | 1 | 0 | 1 |