NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Aerodynamic and rocket-exhaust heating during launch and ascent NASA space vehicle design criteria /Structures/Aerodynamic and rocket exhaust heating during launch and ascent
Document ID
19700009523
Acquisition Source
Legacy CDMS
Document Type
Special Publication (SP)
Date Acquired
September 2, 2013
Publication Date
May 1, 1969
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-SP-8029
Accession Number
70N18828
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available