Krummen, Sven and Sippel, Martin (2017) INVESTIGATION OF THE ASCENT FLIGHT DYNAMICS OF THE SPACELINER CONCEPT AS A NON-SYMMETRIC LAUNCHER CONFIGURATION. Deutscher Luft- und Raumfahrtkongress 2017, 5.-.7. September 2017, München, Deutschland.
![]() |
PDF
670kB |
Official URL: http://www.dlrk2017.dglr.de/nc/paper_download/index.html
Abstract
Determining the flight dynamic characteristics of a space transportation vehicle in its preliminary design phase is a complex task since a large variety of vehicle parameters need to be estimated. For the SpaceLiner vehicle, a concept of a hypersonic suborbital space plane, such an analysis has now been established. In this study a 6 DOF trajectory simulation has been developed to assess the general feasibility of fulfilling the mission requirements during nominal and off-nominal flight conditions.
Item URL in elib: | https://elib.dlr.de/114996/ | |||||||||
---|---|---|---|---|---|---|---|---|---|---|
Document Type: | Conference or Workshop Item (Speech) | |||||||||
Title: | INVESTIGATION OF THE ASCENT FLIGHT DYNAMICS OF THE SPACELINER CONCEPT AS A NON-SYMMETRIC LAUNCHER CONFIGURATION | |||||||||
Authors: |
| |||||||||
Date: | 2017 | |||||||||
Refereed publication: | No | |||||||||
Open Access: | Yes | |||||||||
Gold Open Access: | No | |||||||||
In SCOPUS: | No | |||||||||
In ISI Web of Science: | No | |||||||||
Status: | Published | |||||||||
Keywords: | SpaceLiner, Flight Dynamics, Thrust Vector Control, TRACE, 6 DOF, Trajectory Simulation, Relay Autotuning, Trimmability | |||||||||
Event Title: | Deutscher Luft- und Raumfahrtkongress 2017 | |||||||||
Event Location: | München, Deutschland | |||||||||
Event Type: | national Conference | |||||||||
Event Dates: | 5.-.7. September 2017 | |||||||||
Organizer: | DGLR | |||||||||
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 - Raumfahrzeugsysteme - Systemanalyse Raumtransport | |||||||||
Location: | Bremen | |||||||||
Institutes and Institutions: | Institute of Space Systems > Space Launcher Systems Analysis | |||||||||
Deposited By: | Vormschlag, Nele Marei | |||||||||
Deposited On: | 08 Nov 2017 08:58 | |||||||||
Last Modified: | 31 Jul 2019 20:12 |
Repository Staff Only: item control page