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A Dynamics Study for the Hot Stage Separation of a Multistage Rocket with a Coupled CFD Flight Mechanics Approach

Li, Yi and Eggers, Thino and Reimann, Bodo (2012) A Dynamics Study for the Hot Stage Separation of a Multistage Rocket with a Coupled CFD Flight Mechanics Approach. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, 24. - 28. Sep. 2012, Tours, Frankreich.

Full text not available from this repository.


Item URL in elib:https://elib.dlr.de/84064/
Document Type:Conference or Workshop Item (Speech)
Title:A Dynamics Study for the Hot Stage Separation of a Multistage Rocket with a Coupled CFD Flight Mechanics Approach
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Li, YiUNSPECIFIEDUNSPECIFIED
Eggers, Thinothino.eggers (at) dlr.deUNSPECIFIED
Reimann, Bodobodo.reimann (at) dlr.deUNSPECIFIED
Date:2012
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:Hot stage seperation, flight mechanics, Navier-Stokes
Event Title:18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference
Event Location:Tours, Frankreich
Event Type:international Conference
Event Dates:24. - 28. Sep. 2012
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):R - Shefex III
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Steinberg, Silke
Deposited On:09 Sep 2013 14:04
Last Modified:08 May 2014 23:18

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