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[1] | 
| 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).[2][1] It would mainly qualify the L-15 engine in flight. The engine development project was canceled in 2013.[3]
Characteristics
- Thrust = 15 kN
 - ISP = 321s
 
References
- ^ a b http://www.orbital-eng.com/services/pdfs/spec-liquid-propulsion.pdf
 - ^ 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