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Ignition transients in small hypergolic rockets.Factors influencing rocket ignition pressures and conditions leading to large ignition overpressures, estimating residual propellant in rocket combustor
Document ID
19680040416
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Juran, W.
Stechman, R. C.
Date Acquired
August 4, 2013
Publication Date
March 1, 1968
Publication Information
Publisher: JOURNAL OF SPACECRAFT AND ROCKETS, VOL. 5, P. 288-292.
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 67-515
Report Number: AIAA PAPER 67-515
Meeting Information
Meeting: PROPULSION JOINT SPECIALIST CONFERENCE
Location: WASHINGTON, DC
Start Date: July 17, 1967
End Date: July 21, 1967
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
68A21388
Funding Number(s)
CONTRACT_GRANT: NAS9-150
Distribution Limits
Public
Copyright
Other

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