DEVIANT ABLATION MECHANISM OF NOZZLE THROAT IN SOLID ROCKET MOTORS UNDER ACCELERATION CONDITIONS
IAF Space Propulsion Symposium ; 2020 ; Online
2021
Conference paper
English
BKL: | 55.60 Raumfahrttechnik |
Annular throat rocket nozzle design
TIBKAT | 1961
|Erosion Characteristics of Fluidic Throat in Solid-Rocket Motors
Springer Verlag | 2019
|