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NASA Technical Note: Effect of thrust per element on combustion stability characteristics of hydrogen-oxygen rocket engines (Record no. 566005)

000 -LEADER
fixed length control field	00732nam a22002177a 4500
003 - CONTROL NUMBER IDENTIFIER
control field	OSt
040 ## - CATALOGING SOURCE
Transcribing agency	IIT Kanpur
041 ## - LANGUAGE CODE
Language code of text/sound track or separate title	eng
100 ## - MAIN ENTRY--AUTHOR NAME
Personal name	Salmi, Reino J.
245 ## - TITLE STATEMENT
Title	NASA Technical Note: Effect of thrust per element on combustion stability characteristics of hydrogen-oxygen rocket engines
260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT)
Place of publication	Washington, D.C.
Name of publisher	NASA
Year of publication	1968
300 ## - PHYSICAL DESCRIPTION
Number of Pages	27p.
440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE
Title	NASA Technical Note
440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE
Title	National Aeronautics and Space Administration.
500 ## - GENERAL NOTE
General note	Bound Volume No.101116 Contents TR 7622-7630
500 ## - GENERAL NOTE
General note	Technical Note D-4851-4860
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical Term	Coaxial Injectors -- Oxygen-Hydrogen Rocket Engine
700 ## - ADDED ENTRY--PERSONAL NAME
Personal name	Wanhainen, John P.
700 ## - ADDED ENTRY--PERSONAL NAME
Personal name	Hannum, Ned P.
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type	Technical Report

Holdings
Withdrawn status	Lost status	Damaged status	Not for loan	Collection code	Permanent Location	Current Location	Date acquired	Serial Enumeration / chronology	Accession Number	Koha item type
				COMPACT STORAGE (BASEMENT)	PK Kelkar Library, IIT Kanpur	PK Kelkar Library, IIT Kanpur	2022-08-17	NASA TN D-4851	101116	Technical Report

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