Lessons learned and the recent achievements of a three-stage suborbital rocket production

• Autorzy: Sokołowski Dariusz , Cichocki Maciej

Identyfikatory

DOI

10.37105/sd.194

• Języki publikacji: EN

Abstrakty

EN

The project presented in this article, which consists in designing and launching a three-stage suborbital rocket with a 40 kg payload covers the subjects of the rapid development of a multi-stage proof-of-concept vehicle with a limited time to deploy. These finite resources and a negligible percentage of the technology available tested in-house in advance led to the implementation of chosen, well-known industrial solutions into the concept for a winning strategy. This paper presents the recent achievements and lessons learned from the production phase of the components, namely: the rocket motor, control section compartment, guidance and navigation bay, together with recent achievements and future challenges. This set of components, derived from the project, will fill the gap in the technological chain for future Polish launchers and munition. The three-stage suborbital rocket development project is divided into three phases, which will last a total of three years. The first phase is the conceptual design stage, along with laboratory tests of solutions and subsystems used in the rocket. The second phase consists in flight tests for individual stages, together with the decisive flight of a three-stage rocket made to reach the Kármán line. The final stage involves the commercialization of the developed technology and the creation of a service for carrying research loads of up to 40 kg. The project is valued at approximately USD 5 million. The project is co-financed by the National Centre for Research and Development (NCRD) as part of dedicated support for the Polish space industry.

Słowa kluczowe

EN

rocket; three-stage rocket; missile defense; aircraft defense

PL

rakieta; rakieta trójstopniowa; obrona przeciwrakietowa; obrona przeciwlotnicza

• Wydawca: Centrum Rzeczoznawstwa Budowlanego Sp. z o.o.
• Czasopismo: Safety & Defense
• Rocznik: 2023
• Tom: 1
• Strony: 47--57
• Opis fizyczny: Bibliogr. 15 poz., rys., tab.

Twórcy

autor

Sokołowski Dariusz

• Military Institute of Armament Technology, Zielonka, Poland

• https://orcid.org/0000-0002-8161-6952

autor

Cichocki Maciej

• Military Institute of Armament Technology, Zielonka, Poland

• https://orcid.org/0000-0002-9661-2719+

Bibliografia

• 1. Corliss, W. (1971). NASA Sounding Rockets (NASA SP-4401). NASA. https://history.nasa.gov/SP-4401.pdf
• 2. Faenza, M. G., Boiron, A. J., Haemmerli, B., Lennart, S., Vesteras, T.,& Verberne, O. (2017). Getting Ready for Space: Nammo’s Development of a 30 kN Hybrid Rocket Based Technology Demonstrator. Proceedings of the 7th European Conference For Aeronautics and Space Sciences (EUCASS), Italy, 2017. https://doi.org/10.13009/EUCASS2017-410
• 3. Fitzpatrick, S. (2020). Wallops Range Annual Report. NASA. https://www.nasa.gov/sites/default/files/atoms/files/2020-rmmo-ar.pdf
• 4. Foster, L. R., & Urash, R. G. (1981). The Scout Launch Vehicle Program. The Space Congress Proceedings, USA, 18 (2), 6-48 – 6-77.
• 5. Kaniewski, P. T., Smagowski, P., & Konatowski, S. (2019). Ballistic Target Tracking with Use of Cinetheodolites. International Journal of Aerospace Engineering, 2019 (1). 1-13. https://doi.org/10.1155/2019/3240898
• 6. Marciniak, B., Okninski, A., Bartkowiak, B., & Pakosz M. (2017). Development of the ILR-33 “AMBER” sounding rocket for microgravity experimentation. Aerospace Science and Technology, 73 (11), 19-31. https://doi.org/10.1016/j.ast. 2017.11.034
• 7. Okninski, A. (2017). Multi-disciplinary optimization of single-stage sounding rockets using solid propulsion. Aerospace Science and Technology, 71 (9), 412-419. https://doi.org/10.1016/j.ast.2017.09.039
• 8. Seibert , G. (2006). The History of Sounding Rockets and Their Contribution to European Space Research. ESA.
• 9. Sokolowski, D., Cichocki, M., Wnuk, G., Pyza, M., & Jamroz, E. (2023). Development of a Three-Stage Suborbital Rocket System to Lift Research Payloads. Proceedings of the IEEE Aerospace Conference 2023, USA. https://doi.org/10.1109/AERO55745.2023.10115767
• 10. SpaceForest Ltd. (2023, 04, 12) PERUN. https://spaceforest.pl/perun/ 11. Rasanova, G. (2022). NASA Sounding Rockets Annual Report 2022 (NP-2022-10-892-GSFC). NASA. https://sites.wff.nasa.gov/code810/files/Annual%20Report%202022_web.pdf
• 11. Rasanova, G. (2022). NASA Sounding Rockets Annual Report 2022 (NP-2022-10-892-GSFC NASA. https://sites.wff.nasa.gov/code810/files/Annual%20Report%202022_web.pdf
• 12. Russo, G., Voto, C. (2023). Hyplane: a single-stage suborbital aerospaceplane. CEAS Space Journal, 2023, 1-15. https://doi.org/10.1007/s12567-023-00494-z
• 13. Javier, V. (2016). SENER electromechanical capabilities.
• 14. Wells, H., Whiteley, H., & C.E., K. (1976). Origins of NASA Names (NASA SP-4402). NASA. https://history.nasa.gov/SP-4402/SP-4402.htm.
• 15. Yonemoto, K., & Takahiro, F., & Toshiki, M. & Wang, J. & Choudhuri, A. (2018). Subscale Winged Rocket Development and Application to Future Reusable Space Transportation. INCAS Bulletin, 10 (1), 161-172. https://doi.org/1010.13111/2066-8201.2018.10.1.1

Uwagi

Opracowanie rekordu ze środków MEiN, umowa nr SONP/SP/546092/2022 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2022-2023).