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Red Kite Sounding Rocket Motor - Qualification and Application Spectrum

Scheuerpflug, Frank and Röhr, Thomas Henri and Huber, Thomas and Hargarten, Dorian Amadeus and Kirchhartz, Rainer and Kuhn, Markus and Weigand, Alexander and Berndl, Matthias and Werneth, Josef (2025) Red Kite Sounding Rocket Motor - Qualification and Application Spectrum. Journal of Spacecraft and Rockets, pp. 1-13. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.A36203. ISSN 0022-4650.

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Official URL: https://arc.aiaa.org/doi/10.2514/1.A36203

Abstract

The Red Kite© is a commercially available, solid propellant sounding rocket motor primarily designed as a powerful booster for military surplus and commercial second stages. Typical payloads will range between 200-600 kg. When used in a mission design tailored to microgravity research, typical apogees range between 250-350 km, while the needs of the hypersonic community can be met by a suppressed trajectory design, typically providing horizontal flight at Mach numbers between 6-9 in the altitude band 30-60 km. Following a Phase A definition study in 2017, the German Aerospace Center DLR contracted Bayern Chemie GmbH in 2020 for the development and manufacturing. Subsequent to preliminary design and materials selection phase, ground testing of mechanical, pyrotechnical and electrical subsystems was conducted. Finally, two full scale qualification motors were successfully test-fired in August 2023 at ESRANGE Space Center. Serial production of initially 30 units was initiated and the first motor released for a maiden flight from Andøya Space Center in November 2023, proving the design in flight successfully. The paper gives a summary of the motor performance, aspects of the system design, the qualification program and its application spectrum in active and future sounding rocket vehicles.

Item URL in elib:https://elib.dlr.de/214208/
Document Type:Article
Title:Red Kite Sounding Rocket Motor - Qualification and Application Spectrum
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Scheuerpflug, FrankUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Röhr, Thomas HenriUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Huber, ThomasUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Hargarten, Dorian AmadeusUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Kirchhartz, RainerUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Kuhn, MarkusUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Weigand, AlexanderUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Berndl, MatthiasUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Werneth, JosefUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:18 April 2025
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
Volume:0
DOI:10.2514/1.A36203
Page Range:pp. 1-13
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
De Weck, OlivierUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Dufrene, AaronUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Publisher:American Institute of Aeronautics and Astronautics (AIAA)
ISSN:0022-4650
Status:Published
Keywords:Sounding Rocket, Rocket Motor, Solid Rocket Motor, Hypersonics, Booster
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 - Technologies for sounding rockets
Location: Oberpfaffenhofen
Institutes and Institutions:Space Operations and Astronaut Training
Deposited By: Scheuerpflug, Frank
Deposited On:28 May 2025 08:40
Last Modified:28 May 2025 08:40

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