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Injection and Mixing Processes in High Pressure LOX/GH2 Rocket Combustors.

Mayer, W. and Schik, A. and Schweitzer, C. and Schäffler, M. (1996) Injection and Mixing Processes in High Pressure LOX/GH2 Rocket Combustors. In: 32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Lake Buena Vista, FL, USA, July 1-3, 1996.

Full text not available from this repository.

Abstract

Lampoldshausen 970219.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1996, pages=15,
Title:Injection and Mixing Processes in High Pressure LOX/GH2 Rocket Combustors.
Authors:
AuthorsInstitution or Email of Authors
Mayer, W.UNSPECIFIED
Schik, A.UNSPECIFIED
Schweitzer, C.UNSPECIFIED
Schäffler, M.UNSPECIFIED
Date:1996
Journal or Publication Title:32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Lake Buena Vista, FL, USA, July 1-3, 1996
Series Name:AIAA 96-2620
Status:Published
Keywords:Injector, Atomization, Combustion
HGF - Research field:UNSPECIFIED
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:UNSPECIFIED
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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