发明名称 |
High performance ammonium nitrate propellant |
摘要 |
A high performance propellant having greatly reduced hydrogen chloride emission is disclosed comprising a minor amount of hydrocarbon binder (10-15%) and at least 85% solids including ammonium nitrate as the primary oxidizer (about 40% to 70%), a significant amount (5-25%) powdered metal fuel, such as aluminum, a small amount (5-25%) of ammonium perchlorate as a supplementary oxidizer and optionally a small amount (0-20%) of a nitramine such as HMX.
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申请公布号 |
US4158583(A) |
申请公布日期 |
1979.06.19 |
申请号 |
US19770861390 |
申请日期 |
1977.12.16 |
申请人 |
FROSCH, ROBERT A. ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION, WITH RESPECT TO AN INVENTION OF;ANDERSON, FLOYD A. |
发明人 |
FROSCH, ROBERT A. ADMINISTRATOR OF THE NATIONAL AERONAUTICS AND SPACE ADMINISTRATION, WITH RESPECT TO AN INVENTION OF;ANDERSON, FLOYD A. |
分类号 |
C06B23/00;C06B33/14;C06B45/10;(IPC1-7):C06B45/10 |
主分类号 |
C06B23/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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