Aerodynamic And Rocket-Exhaust Heating During Launch And Ascent,NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

NASA/SP-8029, Aerodynamic And Rocket-Exhaust Heating During Launch And Ascent,NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), NASA Langley Research Center (Hampton, VA, United States), May,1969, pp. 33, Format(s): PDF 2173k

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Aerodynamic and rocket exhaust heating during launch and ascent

Keywords:	thermodynamics and compustion, aerodynamic heating, ascent trajectories, rocket exhaust, spacecraft launching, aeronautical engineering, criteria, exhaust gases, heat transfer, meteorological parameters
CASI Document ID Number:	70N18828
Subjects:	Engineering: Fluid Mechanics and Thermodynamics: Combustion Physics
ID Code:	21
Deposited On:	13 May 2002