Objectives and Achievements of the Hypersonic Flight Experiment STORT
The three-stage rocket configuration of the hypersonic experiment STORT with several scientific payloads concerning hypersonic technologies was launched from the Andøya Space launch site in northern Norway on 26th June 2026 successfully. The third stage performed a suppressed trajectory to increase...
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ftdlr:oai:elib.dlr.de:189284 2024-05-19T07:28:25+00:00 Objectives and Achievements of the Hypersonic Flight Experiment STORT Gülhan, Ali Hargarten, Dorian Amadeus Zurkaulen, Maximilian Klingenberg, Florian Siebe, Frank Reimer, Thomas Di Martino, Giuseppe 2022-09 application/pdf https://elib.dlr.de/189284/ https://elib.dlr.de/189284/1/IAC-22D267x69473%20G%C3%BClhan.pdf en eng https://elib.dlr.de/189284/1/IAC-22D267x69473%20G%C3%BClhan.pdf Gülhan, Ali und Hargarten, Dorian Amadeus und Zurkaulen, Maximilian und Klingenberg, Florian und Siebe, Frank und Reimer, Thomas und Di Martino, Giuseppe (2022) Objectives and Achievements of the Hypersonic Flight Experiment STORT. In: 73rd International Astronautical Congress. 73rd IAC, 2022-09-18 - 2022-09-22, Paris. Über- und Hyperschalltechnologien KP Mobile Raketenbasis Konferenzbeitrag NonPeerReviewed 2022 ftdlr 2024-04-25T01:02:02Z The three-stage rocket configuration of the hypersonic experiment STORT with several scientific payloads concerning hypersonic technologies was launched from the Andøya Space launch site in northern Norway on 26th June 2026 successfully. The third stage performed a suppressed trajectory to increase integral heat load on the structures of payloads. The duration of a flight phase above Mach 8 at altitudes between 30 km and 38 km was more than 60 seconds. The nose and forebody section of the payload is made of the CMC structures. Three canards with a CMC thermal protection were equipped with thermal management experiments to verify the thermal efficiency of these methods. All engineering science experiments like aerothermal heating of the nose and forebody, CMC material response at temperatures above 2200 K, hypersonic thermal management, shock wave boundary layer interaction, CFRP module with cork coating for high temperature applications, high temperature fin leading edge and radiometer sensors provided unique flight data. A reduced in-flight 3 DoF trajectory simulation running on the flight computer determined the ignition time of the third stage which allowed improved experiment conditions in terms of Mach number and apogee altitude even in the presence of external perturbations. Conference Object Andøya Northern Norway German Aerospace Center: elib - DLR electronic library |
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Open Polar |
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German Aerospace Center: elib - DLR electronic library |
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ftdlr |
language |
English |
topic |
Über- und Hyperschalltechnologien KP Mobile Raketenbasis |
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Über- und Hyperschalltechnologien KP Mobile Raketenbasis Gülhan, Ali Hargarten, Dorian Amadeus Zurkaulen, Maximilian Klingenberg, Florian Siebe, Frank Reimer, Thomas Di Martino, Giuseppe Objectives and Achievements of the Hypersonic Flight Experiment STORT |
topic_facet |
Über- und Hyperschalltechnologien KP Mobile Raketenbasis |
description |
The three-stage rocket configuration of the hypersonic experiment STORT with several scientific payloads concerning hypersonic technologies was launched from the Andøya Space launch site in northern Norway on 26th June 2026 successfully. The third stage performed a suppressed trajectory to increase integral heat load on the structures of payloads. The duration of a flight phase above Mach 8 at altitudes between 30 km and 38 km was more than 60 seconds. The nose and forebody section of the payload is made of the CMC structures. Three canards with a CMC thermal protection were equipped with thermal management experiments to verify the thermal efficiency of these methods. All engineering science experiments like aerothermal heating of the nose and forebody, CMC material response at temperatures above 2200 K, hypersonic thermal management, shock wave boundary layer interaction, CFRP module with cork coating for high temperature applications, high temperature fin leading edge and radiometer sensors provided unique flight data. A reduced in-flight 3 DoF trajectory simulation running on the flight computer determined the ignition time of the third stage which allowed improved experiment conditions in terms of Mach number and apogee altitude even in the presence of external perturbations. |
format |
Conference Object |
author |
Gülhan, Ali Hargarten, Dorian Amadeus Zurkaulen, Maximilian Klingenberg, Florian Siebe, Frank Reimer, Thomas Di Martino, Giuseppe |
author_facet |
Gülhan, Ali Hargarten, Dorian Amadeus Zurkaulen, Maximilian Klingenberg, Florian Siebe, Frank Reimer, Thomas Di Martino, Giuseppe |
author_sort |
Gülhan, Ali |
title |
Objectives and Achievements of the Hypersonic Flight Experiment STORT |
title_short |
Objectives and Achievements of the Hypersonic Flight Experiment STORT |
title_full |
Objectives and Achievements of the Hypersonic Flight Experiment STORT |
title_fullStr |
Objectives and Achievements of the Hypersonic Flight Experiment STORT |
title_full_unstemmed |
Objectives and Achievements of the Hypersonic Flight Experiment STORT |
title_sort |
objectives and achievements of the hypersonic flight experiment stort |
publishDate |
2022 |
url |
https://elib.dlr.de/189284/ https://elib.dlr.de/189284/1/IAC-22D267x69473%20G%C3%BClhan.pdf |
genre |
Andøya Northern Norway |
genre_facet |
Andøya Northern Norway |
op_relation |
https://elib.dlr.de/189284/1/IAC-22D267x69473%20G%C3%BClhan.pdf Gülhan, Ali und Hargarten, Dorian Amadeus und Zurkaulen, Maximilian und Klingenberg, Florian und Siebe, Frank und Reimer, Thomas und Di Martino, Giuseppe (2022) Objectives and Achievements of the Hypersonic Flight Experiment STORT. In: 73rd International Astronautical Congress. 73rd IAC, 2022-09-18 - 2022-09-22, Paris. |
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1799472821473116160 |