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Report on trajectory analysis and optimization of the nominal flight trajectory and sensitivities

van Foreest, Arnold (2011) Report on trajectory analysis and optimization of the nominal flight trajectory and sensitivities. Project Report. SART-TN 006/2011, 25 S. (Unpublished)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/
Document Type:Monograph (Project Report)
Title:Report on trajectory analysis and optimization of the nominal flight trajectory and sensitivities
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
van Foreest, ArnoldUNSPECIFIEDUNSPECIFIED
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Status:Unpublished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 Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
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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