The development of a high-capacity instrument module heat transport system, appendixes

Details The development of a high-capacity instrument module heat transport system, appendixes The development of a high-capacity instrument module heat transport system, appendixes

Sep 1981

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1981ladi.reptr.....&link_type=abstract

Final Report Little (Arthur D.), Inc., Cambridge, MA.

Physics

Plasma Physics

Heat Transfer, Instrument Packages, Payloads, Space Platforms, Spacecraft Radiators, Temperature Control, Adiabatic Conditions, Control, Coolants, Heat Pipes, Heat Sinks, Mass Flow, Parameter Identification, Service Life, Two Phase Flow

Scientific paper

Data sheets provide temperature requirements for 82 individual instruments that are under development or planned for grouping on a space platform or pallet. The scientific objectives of these instrument packages are related to solar physics, space plasma physics, astronomy, high energy astrophysics, resources observations, environmental observations, materials processing, and life sciences. System specifications are given for a high capacity instrument module heat transport system to be used with future payloads.

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