Numerical Model for the Prediction of the Regression Rate in Hybrid Rocket Kick-Motors Working with Nitrous Oxide
AIAA SciTech Forum ; 2023 ; National Harbor, Md.; Online
2023
Aufsatz (Konferenz)
Englisch
BKL: | 55.60 Raumfahrttechnik |
Nitrous Oxide Hybrid Rocket Motor Fuel Regression Rate Characterization AIAA Paper
British Library Conference Proceedings | 2007
|