发明名称 |
Lateral exhaust microthruster |
摘要 |
A microthruster having an inverted exhaust system traps burst diaphragm fragments providing a clean exhaust while an exhaust port provides increased back pressure for efficient combustion of a propellant charge in a fuel cell. A converging diverging micronozzle provides a predictable exhaust vector for improved microthrusting well suited for propulsion system on small spacecraft.
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申请公布号 |
US2002166922(A1) |
申请公布日期 |
2002.11.14 |
申请号 |
US20010855005 |
申请日期 |
2001.05.14 |
申请人 |
THE AEROSPACE CORPORATION |
发明人 |
ROBINSON ERNEST Y.;ABRAHAM MARGARET H.;FUQUA PETER D. |
分类号 |
B64G1/26;B64G1/40;F02K9/10;(IPC1-7):B64C27/00;B64C39/00 |
主分类号 |
B64G1/26 |
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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