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Atomization and Breakup of Cryogenic Propellants Under High-Pressure Subcritical and Supercritical Conditions

Mayer, W. and Schik, A. (1998) Atomization and Breakup of Cryogenic Propellants Under High-Pressure Subcritical and Supercritical Conditions. Journal of Propulsion and Power, 14 (5), pp. 835-842.

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Document Type:Article
Additional Information: LIDO-Berichtsjahr=1999,
Title:Atomization and Breakup of Cryogenic Propellants Under High-Pressure Subcritical and Supercritical Conditions
Authors:
AuthorsInstitution or Email of Authors
Mayer, W.UNSPECIFIED
Schik, A.UNSPECIFIED
Date:1998
Journal or Publication Title:Journal of Propulsion and Power
Refereed publication:Yes
In ISI Web of Science:Yes
Volume:14
Page Range:pp. 835-842
Status:Published
Keywords:Liquid rocket engine, rocket combustor, injection, atomization, mixing, combustion
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 13:40

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