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Aerodynamics of the ACCD for the In-AirCapturing of the SpaceLiner Booster

Stappert, Sven (2018) Aerodynamics of the ACCD for the In-AirCapturing of the SpaceLiner Booster. Project Report. SART TN-016/2018. 35 S.

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The SpaceLiner Booster shall perform a re-entry maneuver after separation from the SpaceLiner Passenger stage, followed by a subsonic gliding flight. While in the subsonic flight regime the SpaceLiner is supposed to be captured by a towing aircraft (In-Air-Capturing). Therefore, the towing aircraft shall be equipped with a aerodynamically controllable device that is supposed to capture the SLB. This maneuver shall be calculated and simulated with 6 DOF within the DLR project AKIRA. Prior to this calculation, a valid and adequate aerodynamic model has to be created including static and dynamic derivatives. For this purpose, the software kit Missile DATCOM was used and the results are presented in this report.

Item URL in elib:https://elib.dlr.de/144124/
Document Type:Monograph (Project Report)
Additional Information:Das PDF ist auf Anfrage bei RY-SRT erhältlich!
Title:Aerodynamics of the ACCD for the In-AirCapturing of the SpaceLiner Booster
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Stappert, SvenSven.Stappert (at) dlr.dehttps://orcid.org/0000-0002-8425-2779
Date:December 2018
Refereed publication:No
Open Access:No
Gold Open Access:No
In ISI Web of Science:No
Number of Pages:35
Keywords:SpaceLiner, RLV, ACCD, In-Air-Capturing, 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 12:22
Last Modified:29 Sep 2021 12:22

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