Interface Heat Exchanger System Test.
Abstract
A production Gemini B/Lab Interface Heat Exchanger Assembly was tested to determine (1) its heat transfer characteristics, and (2) system capability to carry the expected heat loads without excessive MOL loop temperature variation. Data was obtained at ground level and at simulated flight environmental conditions. Interface contact forces were at the low and high ends of the installation tolerances. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 29, 1969
- Accession Number
- AD0856674