发明名称 |
Hybrid rocket system and integrated motor for use therein |
摘要 |
A hybrid rocket system and motor includes an oxidant tank communicating with a combustion chamber containing a solid fuel grain. The passage from the oxidant tank to the combustion chamber is obstructed by a fill tube which fills the oxidant tank with oxidant and pressurizes it. Once the tank is full, the fill tube is displaced from the tank-chamber passage to deliver oxidant to the grain and initiate the combustion process. The motor may be an integral part of the rocket, or it may be a modular, expendable or exchangeable cartridge-type device inserted into a reusable body.
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申请公布号 |
US5715675(A) |
申请公布日期 |
1998.02.10 |
申请号 |
US19950383522 |
申请日期 |
1995.02.03 |
申请人 |
ENVIRONMENTAL AEROSCIENCE CORP. |
发明人 |
SMITH, KEVIN W.;KLINE, KOREY R.;SLACK, JR., THEODORE C.;MOSSBERG, ANDREW E. |
分类号 |
F02K9/72;F02K9/76;(IPC1-7):F02K9/72 |
主分类号 |
F02K9/72 |
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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