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Comparison of Facetted and Blunt Lifting Bodies for Re-Entry Flight

Wartemann, Viola and Weihs, Hendrik and Eggers, Thino (2017) Comparison of Facetted and Blunt Lifting Bodies for Re-Entry Flight. 21st AIAA International Space Planes and Hypersonic Systems and Technology Conference, 2017-03-06 - 2017-03-09, Xiamen, China.

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Abstract

The design of a re-entry vehicle strongly depends on the entry strategy of the projected mission. From the aerodynamic point of view, the layout of a hypersonic vehicle is a compromise between a vehicle being blunt enough to reduce the aerodynamic heating and sharp enough to obtain acceptable aerodynamic and propulsive efficiency. The selected flight configurations in this paper are wingless lifting bodies. Two different types of lifting bodies are compared: a sharp and a blunt body. The chosen blunt bicone is one of the ReFEx geometries, which was designed in the frame of the DLR vehicle concept study of ReFEx (Reusability Flight Experiment). The sharp configuration is one of the DLR SHEFEX (SHarp Edge Flight EXperiment) configurations, which is a facetted body with sharp leading edge. The focus of the present study is the discussion of advantages and drawbacks of both concepts with respect to structure and aerodynamics.

Item URL in elib:https://elib.dlr.de/111479/
Document Type:Conference or Workshop Item (Speech)
Additional Information:AIAA-2017-2252
Title:Comparison of Facetted and Blunt Lifting Bodies for Re-Entry Flight
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Wartemann, ViolaAS-RFZ BSUNSPECIFIEDUNSPECIFIED
Weihs, HendrikBT-RSI STUNSPECIFIEDUNSPECIFIED
Eggers, ThinoAS-RFZ BsUNSPECIFIEDUNSPECIFIED
Date:March 2017
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:SHEFEX, SHEFEX III, ReFEx, aerodynamic, Stability and trim characteristics, aerodynamic performance, structure, TPS, re-usable re-entry vehicle
Event Title:21st AIAA International Space Planes and Hypersonic Systems and Technology Conference
Event Location:Xiamen, China
Event Type:international Conference
Event Start Date:6 March 2017
Event End Date:9 March 2017
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 - Shefex III (old)
Location: Braunschweig , Stuttgart
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Institute of Structures and Design > Space System Integration
Deposited By: Wartemann, Viola
Deposited On:29 Mar 2017 11:57
Last Modified:24 Apr 2024 20:16

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