Stanford AA284 2008 Hybrid Rocket - Grain #2 (Final Burn)

Hybrid rocket propulsion system test at Stanford University.


18:16 PDT
Fuel Grain #2. Burn Profile:
T+00.0: Ignition 1 Start
T+00.3: Oxidizer Main Valve open
T+25.3: Oxidizer closed, Helium Quench
T+26.3: Helium Quench shutdown
T+27.3: Ignition 2 Start
T+27.6: Oxidizer Main Valve open
T+29.6: System shutdown

Instrumentation data available by request.

Category:

Science & Technology

Tags:

• rocket
• hybrid
• stanford
• burn
• hot
• fire