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Untersuchung eines Aerospike basierten GOX/GH2 Dual-Mode Thruster Systems für eine kryogene Oberstufe

Gradetzke, Malte (2020) Untersuchung eines Aerospike basierten GOX/GH2 Dual-Mode Thruster Systems für eine kryogene Oberstufe. Institutsseminar, 27.02.2020, Lampoldshausen, D.

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Item URL in elib:https://elib.dlr.de/138925/
Document Type:Conference or Workshop Item (Speech)
Title:Untersuchung eines Aerospike basierten GOX/GH2 Dual-Mode Thruster Systems für eine kryogene Oberstufe
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Gradetzke, MalteDLR, Institut für Raumfahrtantriebe, Lampoldshausen, DUNSPECIFIED
Date:2020
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:aerospike, dual-mode thruster, liquid propellant upper stage, SITVC - Secondary Injection Thrust Vector Control, cold gas reaction control system, APU
Event Title:Institutsseminar
Event Location:Lampoldshausen, D
Event Type:Other
Event Dates:27.02.2020
Organizer:Institut für Raumfahrtantriebe, DLR Lampoldshausen
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:02 Dec 2020 08:44
Last Modified:07 Dec 2020 08:19

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