NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Thermal conditions during typical boost trajectoryAerodynamic heating calculation of Atlas Centaur launch vehicle trajectory
Document ID
19650010305
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Roudebush, W. H. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 2, 2013
Publication Date
March 1, 1965
Subject Category
Thermodynamics And Combustion
Accession Number
65N19906
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TRAJECTORY
ATLAS CENTAUR LAUNCH VEHICLE
AERODYNAMIC HEATING

Available Downloads

There are no available downloads for this record.

Related Records

IDRelationTitle19650010303Collected WorksSealed-form, constrictive-wrapped, external insulation system for liquid-hydrogen tanks of boost vehicles
No Preview Available