EXPERIMENTAL INVESTIGATION OF A FLOW-ORIENTED THROTTLEABLE INJECTOR DESIGNED FOR THROTTLEABLE HYBRID ROCKET MOTOR
IAF Space Propulsion Symposium ; 2020 ; Online
2021
Conference paper
English
BKL: | 55.60 Raumfahrttechnik |
AXISYMMETRIC, THROTTLEABLE NON-GIMBALLED ROCKET ENGINE
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Elsevier | 2021
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