ストレラ (rocket)
 | |
| Function | Satellite launch rocket |
|---|---|
| Production | NPO マシノストロィエニヤ company JSC "Khartron" (control system) [1] |
| Development country |  Russia |
| Size | |
| Overall height | 28.27m [2] |
| Diameter | 2.5m [2] |
| Weight | 105,000 kg [3] |
| The number of the steps | 2 |
| Load capacity | |
| To LEO Payload | 2,000 kg [3] |
| Associated rocket | |
| The series | Universal Rocket |
| The launching results | |
| State | Active play |
| Iba | Baikonur space station |
| The total launching number of times | 3 |
| Success | 3 |
| The first launching | December 5, 2003 |
ストレラ (Russian :Стрела) is a man-made satellite launcher of the Russian Federation. The UR-100N UTTKh intercontinental ballistic missile which I retired from was developed by NPO マシノストロィエニヤ which caught the support of the Russian federal government to a base.
Table of contents
Constitution
With the satellite launch machine that I converted UR-100N UTTKh which is an intercontinental ballistic missile into, it is three steps-type liquid fuel locket. The body is comprised of booster stage, mechanism instrument section (MIS), space head section (SHS), and, to the first step and the second step that are a booster stage, a booster of UR-100N UTTKh is just misappropriated. [4]A promotion system is equipped MIS with and functions as upper section rocket. The MIS misappropriates a post-boost vehicle (PBV) of UR-100N UTTKh. [5]MIS, the part between the step, a payload adapter, a fairing and a payload are included in SHS. There are two kinds of SHS-1 and SHS-2, and fairing shapes are different. [4]
When I launch it from Baikonur space station, I can cast a payload of 1,500 kg into the low orbit of orbit angle of inclination 63 degrees. The orbit angle of inclination is modifiable and depends on the orbital altitude and payload weight to spend. When I use SHS-1, orbit injection is possible with precision within 0.05 degrees at 1%, orbit angle of inclination at altitude. [4]
Similarly, there is ロコット on the rocket based on UR-100N UTTKh, but ロコット is launched by founded ground launching pad whereas ストレラ is fired by a silo under the ground. In addition, ロコット can burn several times and is equipped with high breeze KM of the orbit injection precision whereas it is the diversion of the post-boost beagle which the third step of ストレラ was used for with ICBM, and there is greatly the different point of specifications. ストレラ utilizing an existing body and facilities above the ground is more advantageous on the expense side, but ロコット is superior in the deployment environment of launching ability and the satellite. [5]
| The first step | The second step | |
|---|---|---|
| Full length | 17.2m | 2.8m |
| Diameter | 2.5m | 2.5m |
| Manufacturer | NPO マシノストロィエニヤ company | |
| Display weight | 105t | |
| Oxidizer / fuel | N2O4/UDMH | |
| Mean thrust (vacuum) | 1,870kN | 24kN |
| Specific impulse (vacuum) | 310 seconds | 320 seconds |
| The number of the engines | RD-233 *3, RD-234 *1 | RD-235 *1, RD-236 vernier engine *1 |
| Combustion time | 121 seconds | 183 seconds |
Post-boost beagle APB of the upper section is equipped with one RD-0237 engine and can burn for 500 kg of thrusts, up to 200 seconds.
Launching
It was equipped with a simulated payload on December 5, 2003, and maiden flight was carried out, and the display succeeded [7]. It carried the condor of the radar reconnaissance satellite on June 27, 2013, and close of the second that it was ten years since then was carried out [7]. On December 19, 2014, it carried condor -E for Republic of South Africa, and the third display was carried out. [5]
The display of ストレラ is carried out using the UR-100 silo which existed in Baikonur space station. Originally display was planned by スヴォボードヌイ space station, but the スヴォボードヌイ space station is closed in 2007 without launching ストレラ once, and it is unknown whether launch complex of ストレラ is installed in the ボストチヌイ space station under construction now in the ruins.
| Body number | The launching date and time (UTC) | Form | Iba | Embarkation | Result | Remarks | |
|---|---|---|---|---|---|---|---|
| The first unit [8] | December 5, 2003 06:00 | Baikonur space station 175/59 launching pad | Gruzomaket (condor -E-GVM) | Success | Gruzomaket is a simulated payload of condor -E | ||
| The second unit [7] | June 27, 2013 16:53 | Baikonur space station 175/59 launching pad | Condor | Success | |||
| The third unit [5] | December 19, 2014 4:43 | Baikonur space station 175/59 launching pad | Condor -E | Success | Condor -E is a thing by the ordering of the Republic of South Africa Department of Defense | ||
Footnote
- ^ Control systems for intercontinental ballistic missiles and launch vehicles
- ^ a b Russian Space Web - Strela
- ^ a b Encyclopedia Astronautica (old version) - Strela
- ^ a b c "STRELA ROCKET SPACE COMPLEX". NPO Mashinostroyenia. December 23, 2014 reading.
- ^ a b c d "It is succeeded by ストレラー rocket, display of South African reconnaissance satellite corn dull E". sorae.jp (December 22, 2014). December 22, 2014 reading.
- ^ "Space infrastructure data book rocket world in 2011 (pdf) ". It is pp. corporate judicial person Japan Airlines space industry society 102-103 (March 31, 2011). December 23, 2014 reading.
- ^ a b c "Is it a problem occurrence though I launch Russia, a reconnaissance satellite condor?". sorae.jp (June 30, 2013). December 22, 2014 reading.
- ^ "Gruzomaket." Gunter's Space Page. December 22, 2014 reading.
Outside link
- STRELA ROCKET SPACE COMPLEX
- Silo-Launched Strela Rocket blasts off with Kondor-E Radar Satellite December, 2014 Spaceflight101.com
Allied item
This article is taken from the Japanese Wikipedia ストレラ (rocket)
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