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Instrumentation and Aerothermal Post-Flight Analysis of the Rocket Technology Flight Experiment ROTEX-T

Thiele, Thomas and Gülhan, Ali and Olivier, Herbert (2018) Instrumentation and Aerothermal Post-Flight Analysis of the Rocket Technology Flight Experiment ROTEX-T. Journal of Spacecraft and Rockets. American Institute of Aeronautics and Astronautics (AIAA). ISSN 0022-4650

Full text not available from this repository.

Abstract

Based on experience gathered during the hypersonic flight experiments SHEFEX-I and SHEFEX-II the German Aerospace Center (DLR) performed the flight experiment ROTEX-T (ROcket Technology EXperiment-Transition). ROTEX-T was successfully launched on 19th July 2016 at 06:05 am CEST from the Esrange Space Center near Kiruna in northern Sweden. ROTEX-T was a low cost flight experiment mission without inertial measurement unit, reaction control system or parachute. The payload reached an altitude of 183 kilometers, performed a ballistic re-entry with a total flight time of approximately 446 seconds and was afterwards recovered by helicopter. A unique and modular data acquisition system with sampling rates of 20 Hz, 1 kHz, 10 kHz and 2000 kHz was developed for ROTEX-T to study also instationary aerothermal phenomena.

Item URL in elib:https://elib.dlr.de/116261/
Document Type:Article
Title:Instrumentation and Aerothermal Post-Flight Analysis of the Rocket Technology Flight Experiment ROTEX-T
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Thiele, ThomasThomas.Thiele (at) dlr.deUNSPECIFIED
Gülhan, AliAli.Guelhan (at) dlr.deUNSPECIFIED
Olivier, Herbertshock wave laboratory, rwth aachenUNSPECIFIED
Date:28 June 2018
Journal or Publication Title:Journal of Spacecraft and Rockets
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Publisher:American Institute of Aeronautics and Astronautics (AIAA)
ISSN:0022-4650
Status:Published
Keywords:supersonic, hypersonic, flight experiment, sounding rocket, re-entry, ballistic, boundary layer, transition, laminar, turbulent, heat flux measurement, temperature measurement, pressure measurement, PCB
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:other
DLR - Research area:Raumfahrt
DLR - Program:R - no assignment
DLR - Research theme (Project):R - no assignment
Location: Köln-Porz
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Supersonoc and Hypersonic Technology
Deposited By: Thiele, Thomas
Deposited On:18 Sep 2018 10:20
Last Modified:18 Sep 2018 10:20

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