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van Foreest, Arnold (2011) Report on trajectory analysis and optimization of the nominal flight trajectory and sensitivities. Project Report. SART-TN 006/2011. DLR. 25 S. (Unpublished)
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Abstract
This deliverable presents work done on the optimization of the nominal flight of the SpaceLiner (a flight from Sydney to Western Europe). Optimality is measured with respect to the total take-off mass of the SpaceLiner. The main parameter is therefore propellant mass. A trajectory resulting in lowest propellant requirement (low delta V) is considered the most optimal.
| Item URL in elib: | https://elib.dlr.de/70526/ | ||||||||
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| Document Type: | Monograph (Project Report) | ||||||||
| Title: | Report on trajectory analysis and optimization of the nominal flight trajectory and sensitivities | ||||||||
| Authors: |
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| Date: | July 2011 | ||||||||
| Open Access: | Yes | ||||||||
| Gold Open Access: | No | ||||||||
| In SCOPUS: | No | ||||||||
| In ISI Web of Science: | No | ||||||||
| Number of Pages: | 25 | ||||||||
| Status: | Unpublished | ||||||||
| Keywords: | FAST20XX, SpaceLiner, trajectory | ||||||||
| Institution: | DLR | ||||||||
| Department: | SART (RY-RT) | ||||||||
| 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 - EU Projekte Raumtransport (old) | ||||||||
| Location: | Bremen | ||||||||
| Institutes and Institutions: | Institute of Space Systems > Space Launcher Systems Analysis | ||||||||
| Deposited By: | Foreest, Arnold | ||||||||
| Deposited On: | 22 Aug 2011 07:48 | ||||||||
| Last Modified: | 31 Jul 2019 19:32 |
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