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Effects of steady-state acceleration on combustion characteristics of an aluminized composite solid propellant / by G. Burton Northam.

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Format:
Book
Government document
Author/Creator:
Northam, G. Burton, author.
Contributor:
United States. National Aeronautics and Space Administration, issuing body.
Series:
NASA technical note ; D-4914.
NASA/TN ; D-4914
Language:
English
Subjects (All):
Combustion.
Solid propellants.
Acceleration (Mechanics).
Solid propellant rockets.
Acceleration.
combustion.
acceleration.
Medical Subjects:
Acceleration.
Physical Description:
1 online resource (41 pages) : illustrations.
Place of Publication:
Washington, D.C. : National Aeronautics and Space Administration, December 1968.
Notes:
"December 1968."
Includes bibliographical references (page 14).
Description based on online resource, PDF version; title from title page (NASA, viewed on Apr. 26, 2021)
Other Format:
Print version: Northam, G. Burton. Effects of steady-state acceleration on combustion characteristics of an aluminized composite solid propellant.
OCLC:
150483873

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