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COMPARISON OF TOSCA AND ASTOS OPTIMAL SOLUTIONS FOR THE ASCENT FLIGHT OF A SMALL LAUNCH VEHICLE

da Silveira, Guilherme (2020) COMPARISON OF TOSCA AND ASTOS OPTIMAL SOLUTIONS FOR THE ASCENT FLIGHT OF A SMALL LAUNCH VEHICLE. Project Report. SART TN-007/2020. 25 S.

Full text not available from this repository.

Abstract

This work presents and compares the results obtained with TOSCA/RTS and ASTOS for the optimal trajectory of a small launch vehicle to place a payload into a Low Earth Orbit. The launch vehicle considered here refers to a possible future development of the Brazilian Space Program.

Item URL in elib:https://elib.dlr.de/144134/
Document Type:Monograph (Project Report)
Additional Information:Das PDF ist auf Anfrage bei RY-SRT erhältlich!
Title:COMPARISON OF TOSCA AND ASTOS OPTIMAL SOLUTIONS FOR THE ASCENT FLIGHT OF A SMALL LAUNCH VEHICLE
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
da Silveira, GuilhermeDLRUNSPECIFIEDUNSPECIFIED
Date:26 May 2020
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Number of Pages:25
Status:Published
Keywords:Trajectory optimization, Small launch vehicle, TOSCA, RTS, ASTOS
Department:RY-SRT
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 - Systems Analysis Space Transport (SART)
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Space Launcher Systems Analysis
Deposited By: Vormschlag, Nele Marei
Deposited On:30 Sep 2021 11:57
Last Modified:30 Sep 2021 11:57

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