Erosive Burning of Aluminized Composite Propellants: X-Ray Absorption Measurement, Correlation and Application
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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 |
National Aeronautics and Space Administration |
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テクニカルペーパー
THE EFFECTS OF AL PARTICLE SIZE ON THE BURNING RATE AND RESIDUAL OXIDE IN ALUMINIZED PROPELLANTS
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
National Aeronautics and Space Administration |