发明名称 |
Castable silicone based magnesium fueled propellant |
摘要 |
A castable solid propellant composition suitable for use as a fuel generator for a ducted rocket motor is provided. The binder for the composition is a crosslinked polysiloxane. The polysiloxane polymer which is crosslinked to form the binder has a viscosity measured at 77 DEG F. of from about 12 poise to about 50 poise. The metal fuel for the composition is a mixture of spherical and flake magnesium. The composition contains from about 16% to about 20% polysiloxane binder and from 55% to 63% magnesium fuel. The oxidizer is principally ammonium perchlorate.
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申请公布号 |
US4332631(A) |
申请公布日期 |
1982.06.01 |
申请号 |
US19800164730 |
申请日期 |
1980.06.19 |
申请人 |
HERCULES INCORPORATED |
发明人 |
HERTY, III, CHARLES H.;MCCLENDON, SAMUEL E. |
分类号 |
C06B21/00;C06B33/06;C06B45/10;F02K7/18;(IPC1-7):C06B45/10 |
主分类号 |
C06B21/00 |
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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