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.
Authors
- Paul Elliott (ORCID: https://orcid.org/0000-0002-7511-5684)
- Jamey Jacob (ORCID: https://orcid.org/0000-0002-3376-503X)
- Andrew Walsh (ORCID: https://orcid.org/0000-0001-9506-0855)
- Gavin Stearman
- Chris Rathman
Institutions
- Oklahoma State University Oklahoma City (US)
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