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Fundamentals of Supercritical Mixing and Combustion in LOX/GH2 Rocket Engines

Mayer, W. and Smith, J. (2003) Fundamentals of Supercritical Mixing and Combustion in LOX/GH2 Rocket Engines. In: AIAA Progress in Astronautics and Aeronautics AIAA, 10. AIAA.

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Document Type:Contribution to a Collection
Additional Information: LIDO-Berichtsjahr=2003,
Title:Fundamentals of Supercritical Mixing and Combustion in LOX/GH2 Rocket Engines
Authors:
AuthorsInstitution or Email of Authors
Mayer, W.UNSPECIFIED
Smith, J.UNSPECIFIED
Date:2003
Journal or Publication Title:AIAA Progress in Astronautics and Aeronautics
Refereed publication:Yes
In ISI Web of Science:No
Volume:10
Editors:
EditorsEmail
AIAA, UNSPECIFIED
Publisher:AIAA
Series Name:AIAA
Status:Published
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:16 Sep 2005
Last Modified:06 Jan 2010 14:05

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