THE EFFECT OF FUEL LENGTH ON THE REGRESSION RATE IN SWIRLING-OXIDIZER- FLOW-TYPE HYBRID ROCKET USING A LIQUEFYING FUEL

von Kawabata, Yo
Veröffentlicht in IAF Space Propulsion Symposium (2019 : Washington, DC) IAF Space Propulsion Symposium 2019 ; Volume 2 of 2 (2020)

OCEAN LAUNCH SOLUTION FOR EXPERIMENTAL ROCKETS

von Mori, Takuma
Veröffentlicht in IAF Space Transportation Solutions and Innovations Symposium (2019 : Washington, DC) IAF Space Transportation Solutions and Innovations Symposium 2019 (2020)