Effect of thrust per element on combustion stability characteristics of hydrogen-oxygen rocket engines /

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Bibliographic Details
Author / Creator:	Salmi, Reino J., author.
Imprint:	Washington, D.C. : National Aeronautics and Space Administration, October 1968.
Description:	1 online resource (ii, 27 pages) : illustrations.
Language:	English
Series:	NASA technical note ; TN D-4851 NASA technical note ; D-4851.
Subject:	Rocket engines -- Combustion. Rocket engines -- Thrust. Rocket engines -- Combustion. Rocket engines -- Thrust.
Format:	E-Resource U.S. Federal Government Document Book
URL for this record:	http://pi.lib.uchicago.edu/1001/cat/bib/12675142

Hidden Bibliographic Details
Other authors / contributors:	Wanhainen, John P., author. Hannum, Ned P., author. United States. National Aeronautics and Space Administration, issuing body. Lewis Research Center.
Notes:	"October 1968." Includes bibliographical references (pages 26-27). Description based on online resource, PDF version; title from title page (NASA, viewed on Nov. 6, 2020).
Other form:	Print version: Salmi, Reino J Effect of thrust per element on combustion stability characteristics of hydrogen-oxygen rocket engines
GPO item no.:	0830-H-13 (online)
Govt.docs classification:	NAS 1.14:D-4851

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