发明名称 |
Micropump-based microthruster |
摘要 |
A thruster for providing thrust for spacecraft positioning, which has a propellant reservoir for storing propellant, a reaction chamber for discharging a vapor for providing thrust, a pump module comprising one or more micropumps for drawing propellant from the reservoir and for systematically metering propellant to the reaction chamber in a controlled manner, and a controller for actuating the pump module.
|
申请公布号 |
US6892525(B2) |
申请公布日期 |
2005.05.17 |
申请号 |
US20030456722 |
申请日期 |
2003.06.06 |
申请人 |
HONEYWELL INTERNATIONAL INC. |
发明人 |
GUIHEEN JAMES V.;PALANISAMY THIRUMALAI G. |
分类号 |
F02K9/46;F02K9/56;F02K9/60;F03H1/00;F03H99/00;F04B43/04;(IPC1-7):F02K9/42 |
主分类号 |
F02K9/46 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|