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Photogrammetry of the Map Instrument in a Cryogenic Vacuum EnvironmentMAP Instrument requirements dictated that the instruments Focal Plane Assembly (FPA) and Thermal Reflector System (TRS) maintain a high degree of structural integrity at operational temperatures (< 50K). To verify integrity at these extremes, an elaborate test fixture was constructed to provide a large cryogenic (< 20K) radiative environment and a mobile photogrammetry camera. This paper will discuss MAP's Instrument requirements, how those requirements were verified using photogrammetry, and the test setup used to provide the environment and camera movement needed to verify the instrument's requirements.
Document ID
20000120469
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Hill, M.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Packard, E.
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Pazar, R.
(ManTech Aerospace Greenbelt, MD United States)
Date Acquired
August 19, 2013
Publication Date
October 1, 2000
Subject Category
Instrumentation And Photography
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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