Heating augmentation due to compression pad cavities on the Project Orion CEV heat shield

Heating augmentation due to compression pad cavities on the Project Orion CEV heat shield

Author(s):: Hollis, Brian R. ( NASA Langley Research Center, Hampton, VA )
Publication title:: AIAA meeting papers on disc
Title of ser.:: AIAA Paper : AIAA Applied Aerodynamics Conference
Ser. no.:: 41(2009)
Pub. Year:: 2009
No.:: 2009-3843
Paper no.:: AIAA Paper 2009-3843
Pages:: 18
Pub. info.:: Reston, Va.: American Institute of Aeronautics and Astronautics
ISSN:: 10877215
Language:: English
Call no.:: A07400/200907
Type:: Technical Paper

Details

TDL ID:	ZA00066602
Series ID:	PA00000157
Conf. info. (Name):	AIAA Thermophysics Conference
Conf. info. (Number):	41
Conf. info. (Venue):	San Antonio, Texas
Conf. info. (Date):	2009.06.22-2009.06.25
Note for article:	DOI:10.2514/6.2009-3843 // 41st AIAA Thermophysics Conference 22 - 25 June 2009, San Antonio, Texas

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