COLD GAS EXPERIMENTS ON LINEAR, THRUST-VECTORED AEROSPIKE NOZZLES THROUGH SECONDARY INJECTION
IAF Space Propulsion Symposium ; 2019 ; Washington, DC
2020
Conference paper
English
STUDIES OF FLUIDIC INJECTION THRUST VECTORING IN AEROSPIKE NOZZLES
British Library Conference Proceedings | 2011
|Thrust loss due to design of linear aerospike nozzles
AIAA | 2000
|