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Transient Simulation of Liquid Rocket Engines: A Step Towards a more Educated Propellant Choice between Kerosene and Methane

Manfletti, C. (2004) Transient Simulation of Liquid Rocket Engines: A Step Towards a more Educated Propellant Choice between Kerosene and Methane. In: International Conference on Green Propellants, pp. 1-6. 2nd International Conference on Green Propellants for Space Propulsion, Cagliari, Sardinia, Italy, 7-8 June 2004.

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Item URL in elib:https://elib.dlr.de/1719/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2004,
Title:Transient Simulation of Liquid Rocket Engines: A Step Towards a more Educated Propellant Choice between Kerosene and Methane
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Manfletti, C.UNSPECIFIEDUNSPECIFIED
Date:2004
Journal or Publication Title:International Conference on Green Propellants
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1-6
Editors:
EditorsEmail
ESA, UNSPECIFIED
Status:Published
Event Title:2nd International Conference on Green Propellants for Space Propulsion, Cagliari, Sardinia, Italy, 7-8 June 2004
Organizer:ESA
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 14:10

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