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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.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/1657/
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 AuthorsAuthor's ORCID iD
Mayer, W.UNSPECIFIEDUNSPECIFIED
Smith, J.UNSPECIFIEDUNSPECIFIED
Date:2003
Journal or Publication Title:AIAA Progress in Astronautics and Aeronautics
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:10
Editors:
EditorsEmailEditor's ORCID iD
AIAA, UNSPECIFIEDUNSPECIFIED
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 assignment
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion
Deposited By: DLR-Beauftragter, elib
Deposited On:16 Sep 2005
Last Modified:06 Jan 2010 14:05

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