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Research on High Pressure Cryogenic Combustion

Haidn, O. and Habiballah, M. (2003) Research on High Pressure Cryogenic Combustion. Aerospace Science Technology, 7 (6), pp. 473-491.

Full text not available from this repository.

Abstract

Due to their high specific impulse, Oxygen/Hydrogen systems are often used to increase launcher performance and will probably continue to be preferred option for the next decades. In order to get insight into complex processes involved in the combustion of such propellants, research efforts have been conducted in both France and Germany including theoretical and experimental activities. This article deals with recent progress achived by research teams from both countries in high pressure Oxygen/Hydrogen (O2/H2) combustion systems. In France, the research program was conducted in the framework of the GDR goup including Snecma Moteurs-Rocket Engine Division, Centre National d'Etudes Spatiales (CNES), Centre National de la Recherche Scientifique (CNRS) and ONERA. In Germany, research was conducted in the framework of the national technology program TEKAN involving universities, DLR and Astrium. A close cooperation between teams was made possible through a Memorandum of Understanding (MoU) on research on high pressure cryogaenic combustion.

Document Type:Article
Additional Information: LIDO-Berichtsjahr=2003,
Title:Research on High Pressure Cryogenic Combustion
Authors:
AuthorsInstitution or Email of Authors
Haidn, O.UNSPECIFIED
Habiballah, M.ONERA
Date:2003
Journal or Publication Title:Aerospace Science Technology
Refereed publication:Yes
In ISI Web of Science:Yes
Volume:7
Page Range:pp. 473-491
Status:Published
Keywords:Oxygen/Hydrogen; Combustion device; High pressure; Mascotte; M3; P8; Diagnostics; Modeling
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: Monika Lohmiller
Deposited On:16 Sep 2005
Last Modified:06 Jan 2010 14:04

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