STUDY OF A LOX VAPORIZER FOR AN ALTERING-INTENSITY SWIRLING OXIDIZER FLOW TYPE HYBRID ROCKET

von Watanabe, Kotoha
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Propellants and combustion ; Volume 2 of 2 (2021)

EXPERIMENT ON AIR INTAKE PERFORMANCE OF EJECTOR-JET USING WAX-BASED FUEL HYBRID ROCKET

von Funaki, Shunichi
Veröffentlicht in AIAA Propulsion and Energy Forum (2019 : Indianapolis, Ind.) Inlets, nozzles, and propulsion systems integration (2019)