Results of 10% Thermal Model Test, Nimbus B Sensory Ring: SNAP 19 Expanded Safety Program
Description:
Report describing test results obtained from a thermally scaled model of the Nimbus B spacecraft when tested in the NASA-Ames Research Center 3.5-food Hypersonic Wind Tunnel at a Mach number of 10. Descriptions of the facility, model, and test procedure are described. The test result data is presented and discussed.
Date:
January 1967
Creator:
Shih, C. & Rowe, W. H., Jr.
Item Type:
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Partner:
UNT Libraries Government Documents Department