SNAP 8 CONFIGURATION REENTRY HYPERSONIC HEATING RATES DERIVED FROM A SHOCK TUNNEL TEST.

SNAP 8 CONFIGURATION REENTRY HYPERSONIC HEATING RATES DERIVED FROM A SHOCK TUNNEL TEST. [electronic resource]

Nesdps Office Of Nuclear Energy Space And Defense Power Systems.

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Bibliographic Details
Online Access:	Online Access
Corporate Authors:	North American Aviation, inc. Atomics International Division (Researcher), U.S. Atomic Energy Commission. Division of Technical Information (Researcher)
Format:	Government Document Electronic eBook
Language:	English
Published:	Oak Ridge, Tenn. : Oak Ridge, Tenn. : U.S. Atomic Energy Commission. Division of Technical Information. ; distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy, 1967.
Subjects:	Gases. Reactors. Vessels. Velocity. Propulsion. Shock Tubes. Hypersonics. Shock Waves. Re-entry. Snap-8. Heat Transfer. Mockup. Pipes. Rockets. Space Vehicles. Heating. Tubes. Aerodynamics.

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Call Number:	E 1.99:naa-sr--12383
E 1.99:naa-sr--12383	Available