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Propulsion System Design for Hybrid Sounding Rockets

Dabanovic, Andrija and Martin, Joel and May, Stefan and Eggers, Thino (2022) Propulsion System Design for Hybrid Sounding Rockets. 2nd International Conference on Flight Vehicles, Aerothermodynamics and Re-entry Missions & Engineering (FAR), 19.-23. Jun. 2022, Heilbronn, Germany.

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Item URL in elib:https://elib.dlr.de/189641/
Document Type:Conference or Workshop Item (Speech)
Title:Propulsion System Design for Hybrid Sounding Rockets
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Dabanovic, AndrijaUNSPECIFIEDhttps://orcid.org/0000-0003-4639-9304UNSPECIFIED
Martin, JoelUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
May, StefanUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Eggers, ThinoUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:2022
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Sounding Rocket, Hybrid Propulsion, Subsystem Analysis, Fluid System Design, Computational Fluid Dynamics
Event Title:2nd International Conference on Flight Vehicles, Aerothermodynamics and Re-entry Missions & Engineering (FAR)
Event Location:Heilbronn, Germany
Event Type:international Conference
Event Dates:19.-23. Jun. 2022
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 - Reusable Space Systems and Propulsion Technology
Location: Braunschweig
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Spacecraft, BS
Deposited By: Dabanovic, Andrija
Deposited On:16 Dec 2022 09:08
Last Modified:16 Dec 2022 09:08

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