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

Staged Combustion Cycle Rocket Engine Design Trade-Offs for Future Advanced Passenger Transport

Sippel, Martin and Yamashiro, Ryoma (2012) Staged Combustion Cycle Rocket Engine Design Trade-Offs for Future Advanced Passenger Transport. Association Aéronautique et Astronautique. SPACE PROPULSION 2012,, 7.–10. Mai 2012, BORDEAUX, France.

[img] PDF (Prop2012-2.pdf)
446kB

Abstract

Staged combustion cycle rocket engines with a moderate nominal 16 MPa chamber pressure have been selected as the baseline propulsion system for the visionary intercontinental passenger transport SpaceLiner. Several technical engine design trade-offs are run by numerical simulations and results are pre-sented including: • Fuel rich vs. Full-flow cycle • Useful operational domain in MR • Regenerative cooling options of thrust chamber The engine operational domain is evaluated on launcher system level. The applicability of current European experimental staged combustion technology development (e.g. SCORE-D) on the SpaceLiner propulsion development is assessed.

Item URL in elib:https://elib.dlr.de/78208/
Document Type:Conference or Workshop Item (Speech, Paper)
Title:Staged Combustion Cycle Rocket Engine Design Trade-Offs for Future Advanced Passenger Transport
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Sippel, Martinmartin.sippel (at) dlr.deUNSPECIFIED
Yamashiro, RyomaSpace Transportation System Research and Development Center (JAXA), Tsukuba, JapanUNSPECIFIED
Date:7 May 2012
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Publisher:Association Aéronautique et Astronautique
Status:Published
Keywords:Spaceliner, FAST20XX, STAGED COMBUSTION, Future Advanced Passenger Transport, Cycle Analyse, Design,
Event Title:SPACE PROPULSION 2012,
Event Location:BORDEAUX, France
Event Type:international Conference
Event Dates:7.–10. Mai 2012
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - Raumfahrzeugsysteme - Systemanalyse Raumtransport
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Space Launcher Systems Analysis
Deposited By: Vormschlag, Nele Marei
Deposited On:22 Jan 2013 11:45
Last Modified:31 Jul 2019 19:38

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.