Design and Analysis of a Reusable N2O-Cooled Aerospike Nozzle for Labscale Hybrid Rocket Motor Testing
47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
2011-01-01
Conference paper
Electronic Resource
English
Development of a Reusable Aerospike Nozzle for Hybrid Rocket Motors
British Library Conference Proceedings | 2009
|Results of Labscale Hybrid Rocket Motor investigation
NTRS | 1992
|Results of Labscale Hybrid Rocket Motor investigation
AIAA | 1992
|