APPLICATION TO SATELLITE OF A DIRECT-INJECTION GAS-HYBRID ROCKET SYSTEM USING GLYCIDYL AZIDE POLYMER AND NITROUS OXIDE
IAF Space Propulsion Symposium ; 2020 ; Online
2021
Conference paper
English
BKL: | 55.60 Raumfahrttechnik |
Glycidyl azide polymer combustion modeling
AIAA | 2001
|Nitrous Oxide Resistojets for Hybrid Rocket Application
NTIS | 1998
|Historical development of glycidyl azide polymer
AIAA | 1992
|