Title:
宇宙航空機用能動的熱制御システムおよび方法
Document Type and Number:
Japanese Patent JP4080058
Kind Code:
B2
Abstract:
A spacecraft (10) has combined propulsion and active thermal control systems. A propellant storage tank (20) couples to a pressurant storage tank (18). A working fluid (52) resides in the pressurant storage tank (18) and propels propellant when needed while concurrently acting as a thermal working fluid. The working fluid (52) is expanded then routed to selected cooled components (64). After passing by the cooled components (64), the working fluid (52) is compressed and passed by selected heated components (82). A controller (36) monitors temperature sensors (88) and controls valve assemblies (60, 78) to determine the components (64, 82) to which the working fluid (52) is routed.
Inventors:
Sibnus bass sacar
Robert David Allen
Daniel David Miller
Robert David Allen
Daniel David Miller
Application Number:
JP11020098A
Publication Date:
April 23, 2008
Filing Date:
April 06, 1998
Export Citation:
Assignee:
MOTOROLA INCORPORATED
International Classes:
B64G1/40; B64G1/50
Domestic Patent References:
| JP62041920B2 | ||||
| JP3018777B2 | ||||
| JP2643063B2 | ||||
| JP2175400A | ||||
| JP2839577B2 |
Foreign References:
| US5267605 | ||||
| US5419156 |
Attorney, Agent or Firm:
Mamoru Kuwagaki
Shinsuke Onuki
Masanori Honjo
Shinsuke Onuki
Masanori Honjo