NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Experimental Study of a Hot Structure for a Reentry VehicleA large structural model of a reentry vehicle has been built incorporating design concepts applicable to a radiation-cooled vehicle. Thermal-stress alleviating features of the model are discussed. Environmental tests on the model include approximately 100 cycles of loading at room temperature and 33 cycles of combined loading and-heating up to temperatures of 1,6000 F. Measured temperatures are shown for typical parts of the model. Comparisons are made between experimental and calculated deflections and strains. The structure successfully survived the heating and loading environments.
Document ID
19980223616
Acquisition Source
Headquarters
Document Type
Technical Memorandum (TM)
Authors
Pride, Richard A.
(NASA Langley Research Center Hampton, VA United States)
Royster, Dick M.
(NASA Langley Research Center Hampton, VA United States)
Helms, Bobbie F.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1960
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TM-X-314
Report Number: NASA-TM-X-314
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available