NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

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

Back to Results
ATMOSPHERE ENTRY SIMULATOR AND ITS APPLICATION TO THE DETERMINATION OF ABLATIVE PROPERTIES OF MATERIALS FOR BALLISTIC MISSILESAmes atmosphere entry simulator and its use in determining characteristics of ethyl cellulose as ablative heat shield for ballistic missiles
Document ID
19630002686
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hamaker, F. M. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1960
Subject Category
Electronics
Report/Patent Number
NASA-TM-X-394
Report Number: NASA-TM-X-394
Accession Number
63N12562
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BORANE
SIMULATOR
ETHYL
REENTRY
HEAT SHIELD
PLASTIC MATERIAL
BALLISTIC MISSILE
ABLATING MATERIAL

Related Records

There are no records associated with this record.
No Preview Available