发明名称 |
Satellite control method using single species of bipropellant |
摘要 |
In a spacecraft that controls its position and attitude by a plurality of bipropellant thrusters, controlled ejection and vaporization of a single remaining propellant species generates a thrust force to adjust the spacecraft's position and attitude, thereby allowing an extension of the spacecraft's useful life after the other propellant has been exhausted.
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申请公布号 |
US6024328(A) |
申请公布日期 |
2000.02.15 |
申请号 |
US19960768736 |
申请日期 |
1996.12.18 |
申请人 |
HUGHES ELECTRONICS CORPORATION |
发明人 |
ELLISON, JOHN R. |
分类号 |
B64G1/26;B64G1/40;F02K9/50;(IPC1-7):B64G1/26 |
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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