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Off-Nominal Trajectories of SpaceLiner 7-3

Krummen, Sven and Sippel, Martin (2017) Off-Nominal Trajectories of SpaceLiner 7-3. Project Report. SART TN-014/2017. 68 S.

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This simulation study investigates several ascent trajectories of the SpaceLiner Vehicle under off-nominal conditions. In summary the following scenarios have been simulated considering 3 DOF and 6 DOF motion: 1) Nominal undisturbed ascent trajectory 2) Ascent trajectories with atmospheric disturbances a) Large scale wind profile (HWM93) b) Moderate stochastic gusts (Karman) c) Combined disturbances (HWM93 & Karman) 3) Ascent trajectories under anomaly scenarios a) Reduced Isp of the booster’s SLMEs by -3 s b) Premature stage separation by -6.5 s c) Failure of outermost SLME at Lift-Off d) Failure of outermost SLME at Max-Q The results of these simulation cases are analyzed to assess the technical feasibility of the SpcaeLiner concept

Item URL in elib:https://elib.dlr.de/144106/
Document Type:Monograph (Project Report)
Additional Information:Das PDF ist auf Anfrage bei RY-SRT erhältlich!
Title:Off-Nominal Trajectories of SpaceLiner 7-3
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Krummen, SvenUNSPECIFIEDhttps://orcid.org/0000-0002-4126-688XUNSPECIFIED
Sippel, MartinUNSPECIFIEDhttps://orcid.org/0000-0001-7356-7575UNSPECIFIED
Date:September 2017
Refereed publication:No
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Number of Pages:68
Keywords:SpaceLiner, Off-Nominal Trajectory, 6 DOF
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:29 Sep 2021 12:20
Last Modified:29 Sep 2021 12:20

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