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AN ANALYSIS OF THE INCREASED AERODYNAMIC HEATING TO THE SNAP-27 GRAPHITE LUNAR MODULE FUEL CASK (GLFC) RESULTING FROM THE TITANIUM MOUNTING STRUCTURE
Author
Spahr, H. R.
Published
United States : [publisher not identified], 1968.
[Oak Ridge, Tennessee] : [U.S. Atomic Energy Commission], 1968.
Physical Description
microfiche : negative ; 11 x 15 cm
Full Text available online
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Report Numbers
SC-RR-67-2961
Other Subject(s)
Aerodynamics
Analysis
Fuels
Heat transfer
Heat transfer/analysis in snap-27 fuel capsule and mounting hardware during reentry from lunar flight
Heating
N24300 -engineering-heat transfer & fluid flow
Nesdps office of nuclear energy space and defense power systems
Radioisotopes
Re-entry
Shock waves
Snap-27.
Systems for nuclear auxiliary power (snap-27)/fuel capsule and mounting hardware for, analysis of aerodynamic heating during reentry from lunar flight
Titanium
Collection
U.S. Atomic Energy Commission depository collection.
Note
NSA number: NSA-22-025610
OSTI Identifier 4530272
Research organization: Sandia National Lab. (SNL-NM), Albuquerque, NM (United States).
Funding Information
Sponsored by USDOE.
View MARC record
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