发明名称 |
Integrated arcjet having a heat exchanger and supersonic energy recovery chamber |
摘要 |
A gas ionizable to produce a plasma is introduced into an arcjet whose design includes integration of performance enhancing components in a complimentary manner to significantly improve arcjet performance and capabilities. Major integrated design features include an energy recovery chamber, heat exchanger and by-pass gas flow system which enable the integrated arcjet to operate with minimal frozen flow energy losses, high specific powers and very high thrust levels.
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申请公布号 |
US5640843(A) |
申请公布日期 |
1997.06.24 |
申请号 |
US19950401086 |
申请日期 |
1995.03.08 |
申请人 |
ELECTRIC PROPULSION LABORATORY, INC. ET AL. |
发明人 |
ASTON, GRAEME |
分类号 |
F03H1/00;H05H1/34;(IPC1-7):B23K9/00 |
主分类号 |
F03H1/00 |
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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