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Effects of steady-state acceleration on combustion characteristics of an aluminized composite solid propellant / by G. Burton Northam
Author
Northam, G. Burton
Published
Washington, D.C. : National Aeronautics and Space Administration, December 1968.
Physical Description
1 online resource (41 pages) : illustrations
Additional Creators
United States. National Aeronautics and Space Administration
Access Online
purl.fdlp.gov
Full Text available online
Availability
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Series
NASA technical note ; D-4914
Restrictions on Access
Free-to-read Unrestricted online access
Report Numbers
NAS 1.14:D-4914
Subject(s)
Combustion
Acceleration (physics)
Solid propellants
Acceleration (Mechanics)
Solid propellant rockets
Note
"December 1968."
Bibliography Note
Includes bibliographical references (page 14).
Action Note
committed to retain. Federal Depository Library Program (FDLP). For information on our retention commitment, please contact Microforms and Government Information.
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