DEVIANT ABLATION MECHANISM OF NOZZLE THROAT IN SOLID ROCKET MOTORS UNDER ACCELERATION CONDITIONS
IAF Space Propulsion Symposium ; 2020 ; Online
IAF Space Propulsion Symposium 2020 ; 156-170
2021
Conference paper
English
BKL: | 55.60 Raumfahrttechnik |
Annular throat rocket nozzle design
TIBKAT | 1961
|Non-Eroding Nozzle Throat Material for Rocket Motors with AP-Based Propellant
British Library Conference Proceedings | 1998
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