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Investigation of an Aerospike based GOX / GH2 Dual-Mode-Thruster system for a liquid propellant upper stage

Gradetzke, Malte (2020) Investigation of an Aerospike based GOX / GH2 Dual-Mode-Thruster system for a liquid propellant upper stage. Master's, Universität Stuttgart.

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Item URL in elib:https://elib.dlr.de/137842/
Document Type:Thesis (Master's)
Title:Investigation of an Aerospike based GOX / GH2 Dual-Mode-Thruster system for a liquid propellant upper stage
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Gradetzke, MalteDLR, Institut für Raumfahrtantriebe, Lampoldshausen, DUNSPECIFIED
Date:2020
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:103
Status:Published
Keywords:aerospike, dual-mode thruster, liquid propellant upper stage, SITVC - Secondary Injection Thrust Vector Control, cold gas reaction control system, APU
Institution:Universität Stuttgart
Department:Institut für Raumfahrtsysteme
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):Project Future Fuels
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Propellants
Deposited By: Hanke, Michaela
Deposited On:23 Nov 2020 08:32
Last Modified:23 Nov 2020 08:32

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