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Propellant Atomization in LOX/GH2 Rocket Combustors.

Mayer, W. and Ivancic, B. and Schik, A. and Hornung, U. (1998) Propellant Atomization in LOX/GH2 Rocket Combustors. 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Cleveland, OH, July 13-15, 1998.

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Item URL in elib:https://elib.dlr.de/1366/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=1999,
Title:Propellant Atomization in LOX/GH2 Rocket Combustors.
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Mayer, W.UNSPECIFIEDUNSPECIFIED
Ivancic, B.UNSPECIFIEDUNSPECIFIED
Schik, A.UNSPECIFIEDUNSPECIFIED
Hornung, U.UNSPECIFIEDUNSPECIFIED
Date:1998
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Series Name:AIAA 98-3685
Status:Published
Keywords:Liquid rocket engine, rocket combustor, injection, atomization, mixing, combustion
Event Title:34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Cleveland, OH, July 13-15, 1998
Organizer:American Institute of Aeronautics and Astronautics
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: Lohmiller, Monika
Deposited On:16 Sep 2005
Last Modified:06 Jan 2010 13:40

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