elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Contact | Deutsch
Fontsize: [-] Text [+]

Re-Ignitable Gas Generator Cycle Rocket Engine

Kitsche, Wolfgang (2011) Re-Ignitable Gas Generator Cycle Rocket Engine. In: Proceedings of the 4th European Conference for Aerospace Science. European Conference for Aerospace Science EUCASS, 04.-08.07.2011, St.Petersburg, Russland.

Full text not available from this repository.

Abstract

One of the most essential design features of a liquid rocket propulsion system is the cycle in which the propellant is processed. The strongest European main engine VULCAIN runs on liquid hydrogen and oxygen, it processes the propellant in a gas generator cycle (GGC). The new upcoming upper stage engine for the European launcher ARIANE will be an expander cycle engine. This upper stage engine will have the ability of re-ignition. Re-ignition must be considered as an essential aspect of in-space propulsion. So far the typical application of the GGC-engine is on the first stage, for lift off from ground. This paper presents a solution how to perform re-ignition also on a gas generator cycle engine. The advantages of a GGC-engine can be extended by this design feature and can be interesting especially for engines of high thrust and high specific impulse for orbital transfer and in-space propulsion.

Document Type:Conference or Workshop Item (Speech, Paper)
Title:Re-Ignitable Gas Generator Cycle Rocket Engine
Authors:
AuthorsInstitution or Email of Authors
Kitsche, Wolfgangwolfgang.kitsche@dlr.de
Date:4 July 2011
Journal or Publication Title:Proceedings of the 4th European Conference for Aerospace Science
Status:Published
Keywords:rocket engine, cryogenic, turbo pump, upper stage, re-ignition
Event Title:European Conference for Aerospace Science EUCASS
Event Location:St.Petersburg, Russland
Event Type:international Conference
Event Dates:04.-08.07.2011
Organizer:ESA,CNES,SAFRAN,ISTC,CNRS,ONERA
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):W - Antriebsystemtechnik - Raketenantriebtests (old)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion
Deposited By: Wolfgang Kitsche
Deposited On:07 Dec 2011 13:06
Last Modified:07 Dec 2011 13:06

Repository Staff Only: item control page

Browse
Search
Help & Contact
Informationen
electronic library is running on EPrints 3.3.12
Copyright © 2008-2012 German Aerospace Center (DLR). All rights reserved.