Jump to the main content block

Propulsion research

▼Hybrid Rocket Research
Investigation of the Performance of a 10-Kg-Thrust Hybrid Rocket with HTPB as fuel and GOx as oxidizer.

▼Sounding Rocket

▼Initiation and Propagation of Detonation Wave
Deflagration-to-Detonation Transition (Propane/Oxygen and JP-8/Oxygen Mixtures)
Overdriven Detonation across a mixture (Propane/Oxygen to Propane/Air)