EXPLICIT EXPRESSION TO PREDICT THE EROSIVE BURNING RATE OF SOLID PROPELLANTS
- 著者名:
- Wang, S. ( National Aeronautics and Space Administration )
- 掲載資料名:
- NASA Technical Reports
- 発行年:
- 1986
- 号:
- NASA-TM-88465
- 通号:
- G3/28 43342
- パート:
- NAS1.15:88465
- ペーパー番号:
- N86-28259
- 開始ページ:
- 1
- 終了ページ:
- 9
- 総ページ数:
- 9
- 出版情報:
- National Aeronautics and Space Administration
- 言語:
- 英語
- 資料種別:
- テクニカルペーパー
類似資料:
American Institute of Aeronautics and Astronautics |
7
テクニカルペーパー
SOLID PROPELLANT BURNING RATE MEASUREMENT METHODS USED WITHIN THE NATO PROPULSION COMMUNITY
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
8
テクニカルペーパー
Analytical Expressions for Burning Perimeter and Port Area for a Solid Propellant Finocyl Grain
American Institute of Aeronautics and Astronautics |
3
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 |
American Institute of Aeronautics and Astronautics |
10
テクニカルペーパー
Precision techniques for measuring burning rates of solid propellants during pressure transients
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
11
テクニカルペーパー
Small motor measurement method for determining burning rate of solid rocket propellants
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |