Preliminary Testing for the Oklahoma State University Spaceshot Rocket

Oklahoma State University (OSU) is developing a student-designed, two-stage sounding rocket with the goal of crossing the Kármán line (100 km or 330,000 ft). This paper discusses the preliminary design process of using a series of technology demonstrator rockets to mitigate risk while working up to a spaceshot launch. Subsystems that are being developed and tested include custom filament-wound composite airframes, high-altitude head-end ignition (HEI), and single-break dual-deploy recovery systems. Successful flights have been accomplished up to 28,000 ft, with a launch planned to 100,000 ft in September. The findings highlight the effectiveness of in-house manufacturing techniques and the importance of addressing coning and ignition robustness in high-altitude launches.

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Publication Details

Published
2025-07-16
DOI
https://doi.org/10.2514/6.2025-4002
Primary Topic
Rocket and propulsion systems research
Type
article
Field-Weighted Citation Impact
0.00
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article

Preliminary Testing for the Oklahoma State University Spaceshot Rocket

Paul Elliott, Jamey Jacob, Andrew Walsh, Gavin Stearman et al.
Rocket and propulsion systems research
article

Preliminary Testing for the Oklahoma State University Spaceshot Rocket

Paul Elliott, Jamey Jacob, Andrew Walsh, Gavin Stearman, Chris Rathman
article en

Abstract

Oklahoma State University (OSU) is developing a student-designed, two-stage sounding rocket with the goal of crossing the Kármán line (100 km or 330,000 ft). This paper discusses the preliminary design process of using a series of technology demonstrator rockets to mitigate risk while working up to a spaceshot launch. Subsystems that are being developed and tested include custom filament-wound composite airframes, high-altitude head-end ignition (HEI), and single-break dual-deploy recovery systems. Successful flights have been accomplished up to 28,000 ft, with a launch planned to 100,000 ft in September. The findings highlight the effectiveness of in-house manufacturing techniques and the importance of addressing coning and ignition robustness in high-altitude launches.

Oklahoma State University Oklahoma City (US)
Openalex Percentile: Top 76%
Rocket and propulsion systems research
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