Combustion Mechanisms of Bimodal and Ultra-Fine Aluminum in AP Solid Propellant.
類似資料:
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
2
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 |
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 |
6
テクニカルペーパー
Pressure dependence of burning rate of ammonium perchlorate-hydrocarbon binder solid propellants
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |