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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Main Authors: Gülhan, Ali, Hargarten, Dorian Amadeus, Zurkaulen, Maximilian, Klingenberg, Florian, Siebe, Frank, Reimer, Thomas, Di Martino, Giuseppe
Format: Conference Object
Language:English
Published: 2022
Subjects:
Online Access:https://elib.dlr.de/189284/
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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
collection Unknown
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
genre Andøya
Northern Norway
genre_facet Andøya
Northern Norway
geographic Norway
Andøya
geographic_facet Norway
Andøya
id ftdlr:oai:elib.dlr.de:189284
institution Open Polar
language English
long_lat ENVELOPE(13.982,13.982,68.185,68.185)
op_collection_id ftdlr
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, IAC 2022. 73rd IAC, 2022-09-18 - 2022-09-22, Paris. ISSN 0074-1795.
publishDate 2022
record_format openpolar
spelling ftdlr:oai:elib.dlr.de:189284 2025-06-15T14:07:09+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/ 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, IAC 2022. 73rd IAC, 2022-09-18 - 2022-09-22, Paris. ISSN 0074-1795. Über- und Hyperschalltechnologien KP Mobile Raketenbasis Konferenzbeitrag NonPeerReviewed 2022 ftdlr 2025-06-04T04:58:09Z 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 Unknown Norway Andøya ENVELOPE(13.982,13.982,68.185,68.185)
spellingShingle 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
title 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_short Objectives and Achievements of the Hypersonic Flight Experiment STORT
title_sort objectives and achievements of the hypersonic flight experiment stort
topic Über- und Hyperschalltechnologien
KP
Mobile Raketenbasis
topic_facet Über- und Hyperschalltechnologien
KP
Mobile Raketenbasis
url https://elib.dlr.de/189284/