The Strela carrier rocket | |
| Function | Orbital carrier rocket |
|---|---|
| Manufacturer | NPO Mashinostroyeniya, JSC "Khartron", Ukraine (control system) |
| Country of origin | Russia |
| Size | |
| Height | 28.3 metres (93 ft) |
| Diameter | 2.5 metres (8.2 ft) |
| Mass | 105,000 kilograms (231,000 lb) |
| Stages | 3 |
| Capacity | |
| Payload to LEO | |
| Mass | 1,400 kilograms (3,100 lb) |
| Associated rockets | |
| Family | Universal Rocket |
| Launch history | |
| Status | Inactive |
| Launch sites | Baikonur Cosmodrome |
| Total launches | 3 |
| Success(es) | 3 |
| First flight | 5 December 2003 |
| First stage | |
| Diameter | 2.5 m (8.2 ft) |
| Powered by | 3 RD-0233 (15D95) 1 RD-0234 (15D96) |
| Maximum thrust | 2,080 kN (470,000 lbf) |
| Specific impulse | 310 s |
| Burn time | 120 seconds |
| Propellant | N2O4 / UDMH |
| Second stage | |
| Diameter | 2.5 m (8.2 ft) |
| Powered by | 1 RD-0235 (15D113) 1 RD-0236 (15D114) |
| Maximum thrust | 255.76 kN (57,500 lbf) |
| Specific impulse | 310 s |
| Burn time | 180 seconds |
| Propellant | N2O4 / UDMH |
| Third stage – APB (Agregatno-Priborny Otsek) | |
| Powered by | 1 RD-0237 (15D114) |
| Maximum thrust | 4.90 kilonewtons (1,100 lbf) |
| Specific impulse | 200 s |
| Propellant | N2O4 / UDMH |
| External images | |
|---|---|
Strela (Russian: Стрела, arrow) 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.
Strela was originally planned to be launched from the Svobodny Cosmodrome, with test launches being conducted from existing UR-100 silos at the Baikonur Cosmodrome. Svobodny was closed in 2007, without seeing any Strela launches. It is unclear whether a Strela launch complex will be incorporated into the Vostochny Cosmodrome.
Strela differs from the Rockot, which is also derived from the UR-100, in that it has undergone fewer modifications, such as the absence of an additional Briz-KM upper stage, as used on the Rockot. However it is equipped with a repurposed APB as upper stage, which was originally a maneuvrable warhead "bus" from MIRV system of UR-100 missile. It is also launched from silos, whereas the Rockot is launched from flat pads.
| Date (UTC) | Type | Launch site | Payload | Payload type | Outcome |
|---|---|---|---|---|---|
| 5 December 2003, 06:00 | Strela | Ba LC175 | Gruzomaket | test launch | Success |
| 27 June 2013, 16:53 | Strela | Ba LC175 | Kondor | research satellite | Success |
| 19 December 2014, 04:43 | Strela | Ba LC175 | Kondor-E | research satellite | Success |
