Strela The Strela carrier rocket |
| Function | Orbital carrier rocket |
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| Manufacturer | NPO Mashinostroyeniya, JSC "Khartron", Ukraine (control system)[1] |
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| Country of origin | Russia |
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| Size |
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| Height | 28.3 metres (93 ft)[2] |
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| Diameter | 2.5 metres (8.2 ft)[2] |
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| Mass | 105,000 kilograms (231,000 lb)[3] |
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| Stages | 2 |
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| Capacity
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| Payload to LEO | 1,400 kilograms (3,100 lb)[3] |
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|
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| Associated rockets |
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| Family | Universal Rocket |
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| Launch history |
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| Status | Inactive |
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| Launch sites | Baikonur Cosmodrome |
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| Total launches | 3 |
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| Successes | 3 |
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| First flight | 5 December 2003 |
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|
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| First stage |
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| Diameter | 2.5 m (8.2 ft)[4] |
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| Engines | 3 RD-0233 (15D95) 1 RD-0234(15D96)[5][6] |
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| Thrust | 2,080 kN (470,000 lbf)[7][8] |
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| Specific impulse | 310s[7] |
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| Burn time | 120 seconds |
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| Fuel | N 2O 4 / UDMH |
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| Second stage |
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| Diameter | 2.5 m (8.2 ft)[4] |
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| Engines | 1 RD-0235 (15D113) 1 RD-0236 (15D114)[5][6] |
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| Thrust | 255.76 kN (57,500 lbf)[9][10] |
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| Specific impulse | 310s[9] |
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| Burn time | 180 seconds |
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| Fuel | N 2O 4 / UDMH |
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| Third stage – APB (Agregatno-Priborny Otsek)[2] |
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| Engines | 1 RD-0237[11] |
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| Thrust | 4.90 kilonewtons (1,100 lbf)[11] |
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| Specific impulse | 200 s sec[11] |
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| Fuel | N 2O 4 / UDMH |
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External images Strela launch vehicle launch 19.12.2014 |
Strela launch vehicle launch 19.12.2014 |
Strela launch vehicle launch 19.12.2014 |
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,[12] and a second one on 19 December 2014.[13][14]
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, which is being built on the site of Svobodny.[citation needed]
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 designed to deliver nuclear warheads. It is also launched from silos, whereas the Rockot is launched from flat pads.[citation needed]
Launch history
| 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
|
See also
- Comparison of orbital launchers families
- Comparison of orbital launch systems
- Dnepr rocket
References
- ↑ "Control systems for intercontinental ballistic missiles and launch vehicles". JSC "Khartron". http://arkos.kharkov.ua/sumbr_e.php.
- ↑ 2.0 2.1 2.2 Zak, Anatoly. "Strela launcher". http://www.russianspaceweb.com/strela.html.
- ↑ 3.0 3.1 Wade, Mark. "Strela". Encyclopedia Astronautica. http://www.astronautix.com/lvs/strela.htm.
- ↑ 4.0 4.1 Zak, Anatoly. "UR-100N Family". http://www.russianspaceweb.com/ur100n.html.
- ↑ 5.0 5.1 "RD-0233, RD-0234, RD-0235, RD-0236, RD-0237. Intercontinental ballistic missiles RS-18". KBKhA. http://www.kbkha.ru/?p=8&cat=10&prod=47.
- ↑ 6.0 6.1 "Rockot Launch Vehicle". Khrunichev State Research and Production Space Center. http://www.khrunichev.ru/main.php?id=43.
- ↑ 7.0 7.1 Wade, Mark. "RD-0233". http://www.astronautix.com/engines/rd0233.htm.
- ↑ Wade, Mark. "RD-0234". http://www.astronautix.com/engines/rd0234.htm.
- ↑ 9.0 9.1 Wade, Mark. "RD-0235". http://www.astronautix.com/engines/rd0235.htm.
- ↑ Wade, Mark. "RD-0236". http://www.astronautix.com/engines/rd0236.htm.
- ↑ 11.0 11.1 11.2 Wade, Mark. "RD-0237". http://www.astronautix.com/engines/rd0237.htm.
- ↑ Graham, William. "Russian Strela rocket launches Kondor satellite". NasaSpaceFlight.com. http://www.nasaspaceflight.com/2013/06/strela-rocket-launch-kondor-e/.
- ↑ Graham, William. "Russian Strela rocket launches Kondor-E". NasaSpaceFlight.com. http://www.nasaspaceflight.com/2014/12/russian-strela-launch-kondor-e/.
- ↑ "Strela launcher". http://www.russianspaceweb.com/strela.html.
Universal Rocket family |
|---|
| Variants | | Main series |
- UR-100
- UR-200
- UR-500
- UR-700
- UR-900
|
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| UR-100 family |
- UR-100
- UR-100N
- Rokot
- Strela
|
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| UR-500 family |
- UR-500
- Proton
- Proton-K
- Proton-M
- Proton Medium
- Proton Light
|
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|
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| Launch sites | | Baikonur |
- Site 81
- Site 175
- Site 200
|
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| Plesetsk | |
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|
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| Launches |
- List of Proton launches
- 1965–1969
- 1970–1979
- 1980–1989
- 1990–1999
- 2000–2009
- 2010–2019
- 2020–2029
|
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|
Soviet, Russian, and Ukrainian launch vehicles |
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| Active | |
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| In development |
- Angara 1.2
- Cyclone-4M
- Irtysh
- Proton
- Soyuz-7
|
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| Retired |
- Dnepr
- Energia
- Kosmos
- N1
- R-7
- Luna
- Molniya
- Polyot
- Soyuz
- Soyuz/Vostok
- Sputnik
- Voskhod
- Vostok
- R-29
- Start-1
- Tsyklon
- UR
- UR-500
- Proton-K
- Rokot
- Strela
- Zenit
|
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Orbital launch systems |
|---|
- List of orbital launch systems
- Comparison of orbital launch systems
|
| Current |
- Angara
- Antares 230+
- Ariane 5
- Atlas V
- Delta IV Heavy
- Electron
- Epsilon
- Falcon 9 Block 5
- Falcon Heavy
- GSLV
- H-IIA
- H-IIB
- Hyperbola-1
- Jielong 1
- Kuaizhou
- Kaituozhe 2
- Long March
- 2C
- 2D
- 2F
- 3A
- 3B/E
- 3C
- 4B
- 4C
- 5
- 6
- 7
- 11
- Minotaur
- OS-M1
- Pegasus XL
- Proton-M
- PSLV
- Safir
- Shavit
- Simorgh
- Soyuz-2
- 2.1a / STA
- 2.1b / STB
- 2-1v
- Unha
- Vega
- Zenit
- Zhuque-1
|
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| In development |
- Angara 1.2
- Ariane 6
- Bloostar
- Cyclone-4M
- Eris
- Firefly Alpha
- Beta
- H3
- Hyperbola-2
- Irtysh
- Kuaizhou
- LauncherOne
- Long March
- Miura 5
- New Glenn
- New Line 1
- Nuri
- OmegA
- OS-M2
- OS-M4
- Orbex Prime
- SLS
- Soyuz-7
- SSLV
- Starship
- Terran 1
- Vega C
- Vega E
- Vulcan
- Zero
- Zhuque-2
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| Retired | |
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| Classes |
- Sounding rocket
- Small-lift launch vehicle
- Medium-lift launch vehicle
- Heavy-lift launch vehicle
- Super heavy-lift launch vehicle
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- Symbol † indicates projects terminated before a successful orbital launch
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