Flight testing of a university based H2O2/HDPE hybrid sounding rocket at KAIST
53rd AIAA/SAE/ASEE Joint Propulsion Conference
2017-01-01
Conference paper
Electronic Resource
English
Flight Testing of a University Based H~2O~2/HDPE Hybrid Sounding Rocket at KAIST (AIAA 2017-4901)
British Library Conference Proceedings | 2017
|Design of a small H2O2/HTPB hybrid sounding rocket motor
AIAA | 1996
|Flight analysis of sounding rocket
Engineering Index Backfile | 1938
|NTRS
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