Design and Experimental Validation of a Mass-Efficient Pancake Hybrid Rocket Motor with Vortex-Induced Flow for In-Space Application

Design and Experimental Validation of a Mass-Efficient Pancake Hybrid Rocket Motor with Vortex-Induced Flow for In-Space Application

Item #:: 083090-0145
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DOI: https://doi.org/10.52202/083090-0145
Author(s): Beste Boybasi, Mehmet Kemal Ergin
Pages: 1310-1319 (10 pages)
Format: PDF Paper Download
Conference: IAF Space Propulsion Symposium
Date/Location: Held 29 September - 3 October 2025, Sydney, Australia.
Publisher: International Astronautical Federation (IAF)

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DOI: https://doi.org/10.52202/083090-0145
Author(s): Beste Boybasi, Mehmet Kemal Ergin
Pages: 1310-1319 (10 pages)
Format: PDF Paper Download
Conference: IAF Space Propulsion Symposium
Date/Location: Held 29 September - 3 October 2025, Sydney, Australia.
Publisher: International Astronautical Federation (IAF)