Instrumentation and Aerothermal Post-Flight Analysis of the Rocket Technology Flight Experiment ROTEX-T
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 Spac...
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Online Access: | https://elib.dlr.de/116261/ https://doi.org/10.2514/1.A34129 |
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ftdlr:oai:elib.dlr.de:116261 2023-12-31T10:08:55+01:00 Instrumentation and Aerothermal Post-Flight Analysis of the Rocket Technology Flight Experiment ROTEX-T Thiele, Thomas Gülhan, Ali Olivier, Herbert 2018-06-29 https://elib.dlr.de/116261/ https://doi.org/10.2514/1.A34129 unknown American Institute of Aeronautics and Astronautics (AIAA) Thiele, Thomas und Gülhan, Ali und Olivier, Herbert (2018) Instrumentation and Aerothermal Post-Flight Analysis of the Rocket Technology Flight Experiment ROTEX-T. Journal of Spacecraft and Rockets, 55 (5), Seiten 1050-1073. American Institute of Aeronautics and Astronautics (AIAA). doi:10.2514/1.A34129 <https://doi.org/10.2514/1.A34129>. ISSN 0022-4650. Über- und Hyperschalltechnologien KP Zeitschriftenbeitrag PeerReviewed 2018 ftdlr https://doi.org/10.2514/1.A34129 2023-12-04T00:24:15Z 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. Article in Journal/Newspaper Kiruna Northern Sweden German Aerospace Center: elib - DLR electronic library Journal of Spacecraft and Rockets 55 5 1050 1073 |
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German Aerospace Center: elib - DLR electronic library |
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Über- und Hyperschalltechnologien KP |
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Über- und Hyperschalltechnologien KP Thiele, Thomas Gülhan, Ali Olivier, Herbert Instrumentation and Aerothermal Post-Flight Analysis of the Rocket Technology Flight Experiment ROTEX-T |
topic_facet |
Über- und Hyperschalltechnologien KP |
description |
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. |
format |
Article in Journal/Newspaper |
author |
Thiele, Thomas Gülhan, Ali Olivier, Herbert |
author_facet |
Thiele, Thomas Gülhan, Ali Olivier, Herbert |
author_sort |
Thiele, Thomas |
title |
Instrumentation and Aerothermal Post-Flight Analysis of the Rocket Technology Flight Experiment ROTEX-T |
title_short |
Instrumentation and Aerothermal Post-Flight Analysis of the Rocket Technology Flight Experiment ROTEX-T |
title_full |
Instrumentation and Aerothermal Post-Flight Analysis of the Rocket Technology Flight Experiment ROTEX-T |
title_fullStr |
Instrumentation and Aerothermal Post-Flight Analysis of the Rocket Technology Flight Experiment ROTEX-T |
title_full_unstemmed |
Instrumentation and Aerothermal Post-Flight Analysis of the Rocket Technology Flight Experiment ROTEX-T |
title_sort |
instrumentation and aerothermal post-flight analysis of the rocket technology flight experiment rotex-t |
publisher |
American Institute of Aeronautics and Astronautics (AIAA) |
publishDate |
2018 |
url |
https://elib.dlr.de/116261/ https://doi.org/10.2514/1.A34129 |
genre |
Kiruna Northern Sweden |
genre_facet |
Kiruna Northern Sweden |
op_relation |
Thiele, Thomas und Gülhan, Ali und Olivier, Herbert (2018) Instrumentation and Aerothermal Post-Flight Analysis of the Rocket Technology Flight Experiment ROTEX-T. Journal of Spacecraft and Rockets, 55 (5), Seiten 1050-1073. American Institute of Aeronautics and Astronautics (AIAA). doi:10.2514/1.A34129 <https://doi.org/10.2514/1.A34129>. ISSN 0022-4650. |
op_doi |
https://doi.org/10.2514/1.A34129 |
container_title |
Journal of Spacecraft and Rockets |
container_volume |
55 |
container_issue |
5 |
container_start_page |
1050 |
op_container_end_page |
1073 |
_version_ |
1786841866611720192 |