Development of a LOX/RP-1 Vortex Combustion Cold-Wall Thrust Chamber Assembly.
類似資料:
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
11
テクニカルペーパー
Experimental investigation of a vortex-driven high-regression rate hybrid rocket engine
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
テクニカルペーパー
Cold Flow Analysis of a Vortex Chamber Engine for Gelled Propellant Combustor Applications
American Institute of Aeronautics and Astronautics |