The Development of a high-capacity instrument module heat transport system [microform] : appendixes : final report to National Aeronautics and Space Administration, Goddard Space Flight Center / prepared by Arthur D. Little, Inc.

"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 astroph...

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Bibliographic Details
Corporate Authors: United States. National Aeronautics and Space Administration, Arthur D. Little, Inc, Goddard Space Flight Center
Format: Government Document Microfilm Book
Language:English
Published: Greenbelt, Md. : National Aeronautics and Space Administration, Goddard Space Flight Center, [1981]
Series:NASA contractor report ; NASA CR-175260.
Subjects:

MARC

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520 |a "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."--NASA Technical Reports Server web site. 
533 |a Microfiche.  |b [Washington, D.C.? :  |c National Aeronautics and Space Administration],  |d 1984.  |e 2 microfiches ; 11 x 15 cm. 
520 0 |a 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. 
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