VS-15
| Function | Sounding rocket |
|---|---|
| Country of origin | Brazil |
| Size | |
| Stages | 1 |
| Launch history | |
| Status | Cancelled in 2013 |
| Launch sites | Alcântara |
| First stage - L-15 | |
| Engines | 1 |
| Thrust | 15 kN |
| Specific impulse | 321 s |
| Propellant | LOX/RP-1 |
The VS-15 is a Brazilian sounding rocket. It consists of a single, liquid fuel recoverable stage, based on the new L-15 engine (with 15 kN of thrust). It would mainly qualify the L-15 engine in flight. The engine development project was canceled in 2013.
Characteristics
- Thrust = 15 kN
- ISP = 321s
References
- 1 2 http://www.orbital-eng.com/services/pdfs/spec-liquid-propulsion.pdf [dead link]
- ↑ Gomes Paula, Victor Magno. "A TECNOLOGIA DE PROPULSÃO LÍQUIDA NO BRASIL" (PDF) (in Brazilian Portuguese). Archived from the original (PDF) on 2013-03-19. Retrieved 2012-10-05.
- ↑ Instituto de Aeronáutica e Espaço
| Satellites |
| ||||
|---|---|---|---|---|---|
| Sounding rockets |
| ||||
| Launch vehicles |
| ||||
| Launch sites | |||||
| Organisation | |||||
| Missions | |||||
| International programs |
| ||||
 | This Brazilian science article is a stub. You can help Wikipedia by adding missing information. |
 | This rocketry article is a stub. You can help Wikipedia by adding missing information. |