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

Cycle Analysis and Feasibility Evaluation of Pump Fed Hybrid Propulsion System

Dos Santos Hahn, Robson Henrique and Waxenegger-Wilfing, Günther and Schmierer, Christian and Deeken, Jan (2018) Cycle Analysis and Feasibility Evaluation of Pump Fed Hybrid Propulsion System. In: proceedings - Space Propulsion 2018. Space Propulsion 2018, 14. - 18 Mai 2018, Seville, Spain.

[img] PDF - Only accessible within DLR

Item URL in elib:https://elib.dlr.de/124733/
Document Type:Conference or Workshop Item (Speech)
Title:Cycle Analysis and Feasibility Evaluation of Pump Fed Hybrid Propulsion System
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Dos Santos Hahn, Robson HenriqueUNSPECIFIEDhttps://orcid.org/0000-0002-2389-2043UNSPECIFIED
Waxenegger-Wilfing, GüntherUNSPECIFIEDhttps://orcid.org/0000-0001-5381-6431UNSPECIFIED
Schmierer, ChristianUNSPECIFIEDhttps://orcid.org/0000-0002-5960-4592UNSPECIFIED
Deeken, JanUNSPECIFIEDhttps://orcid.org/0000-0002-5714-8845UNSPECIFIED
Journal or Publication Title:proceedings - Space Propulsion 2018
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Keywords:hybrid Motor, turbopump, rocket engine, cycle analysis
Event Title:Space Propulsion 2018
Event Location:Seville, Spain
Event Type:international Conference
Event Dates:14. - 18 Mai 2018
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Raumfahrzeugsysteme - Systemanalyse Raumtransport (old)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion
Institute of Space Propulsion > Propellants
Deposited By: Hanke, Michaela
Deposited On:19 Dec 2018 09:19
Last Modified:19 Dec 2018 09:19

Repository Staff Only: item control page

Help & Contact
electronic library is running on EPrints 3.3.12
Website and database design: Copyright © German Aerospace Center (DLR). All rights reserved.