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Component Modeling for Rocket Engine Cycle Analysis

Herbertz, A. (2016) Component Modeling for Rocket Engine Cycle Analysis. Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, 14 (ists30), pp. 119-127. JSASS. ISSN 1884-0485

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Item URL in elib:https://elib.dlr.de/116783/
Document Type:Article
Title:Component Modeling for Rocket Engine Cycle Analysis
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Herbertz, A.Institute of Space Propulsion, German Aerospace Center, Lampoldshausen, DUNSPECIFIED
Date:2016
Journal or Publication Title:Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:14
Page Range:pp. 119-127
Publisher:JSASS
ISSN:1884-0485
Status:Published
Keywords:Systems Analysis, space Propulsion, gas Generator cycle, Expander bleed cycle
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):Systemanalyse Raumtransport (SART)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hanke, Michaela
Deposited On:11 Dec 2017 13:40
Last Modified:30 May 2019 22:07

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