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Propellant Injection in a Liquid Oxygen/Gaseous Hydrogen Rocket Engine

Mayer, W. and Tamura, H. (1996) Propellant Injection in a Liquid Oxygen/Gaseous Hydrogen Rocket Engine. Journal of Propulsion and Power, Vol.12 (No. 6), pp. 1137-1147.

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Document Type:Article
Additional Information: LIDO-Berichtsjahr=1996,
Title:Propellant Injection in a Liquid Oxygen/Gaseous Hydrogen Rocket Engine
Authors:
AuthorsInstitution or Email of Authors
Mayer, W.UNSPECIFIED
Tamura, H.National Aerospace Laboratory, Miyagi, Japan
Date:1996
Journal or Publication Title:Journal of Propulsion and Power
Refereed publication:Yes
In ISI Web of Science:Yes
Volume:Vol.12
Page Range:pp. 1137-1147
Status:Published
Keywords:Injection, Rocket Combustor, Atomization, Flow Visualization
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:Space
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):E -- no assignement
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion
Deposited By: elib DLR-Beauftragter
Deposited On:02 Apr 2006
Last Modified:27 Apr 2009 05:40

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