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Modeling and Test Results for Two Loop Heat Pipes with a Freeze-Tolerant Condenser Lockheed Martin Space Systems Company
- Format:
- Book
- Conference/Event
- Author/Creator:
- Ambrose, Jay, author.
- Conference Name:
- International Conference On Environmental Systems (2000-07-10 : Toulouse, France)
- Language:
- English
- Physical Description:
- 1 online resource cm
- Place of Publication:
- Warrendale, PA SAE International 2000
- Summary:
- This paper describes modeling and test results for a two Loop Heat Pipes (LHP) with a condenser designed to be used in a deployable spacecraft radiator system. These units were provided by the two major commercial US vendors of LHPs. The condenser used is a freeze-tolerant, parallel-flow design based on the International Space Station (ISS) deployable radiator design. This condenser allows the deployable radiator to be utilized without freeze-protection heaters
- Notes:
- Vendor supplied data
- Publisher Number:
- 2000-01-2411
- Access Restriction:
- Restricted for use by site license
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