| タイトル | High performance ammonium nitrate propellant |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790020171 |
| 著者（英） | Anderson, F. A. |
| 著者所属（英） | NASA Pasadena Office; Jet Propulsion Lab., California Inst. of Tech. |
| 発行日 | 1979-06-19 |
| 言語 | eng |
| 内容記述 | A high performance propellant having greatly reduced hydrogen chloride emission is presented. It is comprised of: (1) a minor amount of hydrocarbon binder (10-15%), (2) at least 85% solids including ammonium nitrate as the primary oxidizer (about 40% to 70%), (3) a significant amount (5-25%) powdered metal fuel, such as aluminum, (4) a small amount (5-25%) of ammonium perchlorate as a supplementary oxidizer, and (5) optionally a small amount (0-20%) of a nitramine. |
| NASA分類 | PROPELLANTS AND FUELS |
| レポートNO | 79N28342 |
| 権利 | No Copyright |
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