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Solid Rocket Boosters Separation System Development for the ILR-33 Amber 2K Rocket

Treść / Zawartość
Identyfikatory
Warianty tytułu
Języki publikacji
EN
Abstrakty
EN
The paper presents the development process of the solid rocket boosters (SRBs) separation system of the ILR-33 AMBER 2K rocket. A redesign of the system was required due to the development of new, larger SRBs. The main system requirements were transmission of forces and moments between the SRBs and the main stage, execution of the separation process at a given moment in flight and mechanical integration simplification. A set of aerodynamics calculations were performed. With the use of computational fluid dynamics software, forces acting on the booster during separation for several angles of attack, as well as the critical booster deflection angle, have been determined. Next, a mathematical model was created to define the load spectrum acting on the system during the flight and separation phases, covering both static and dynamic loads. All the internal and external force sources were considered. A series of motion dynamics simulations were conducted for representative flight cases. Then, the system operational parameters were verified with the use of dedicated ground test facilities. Necessary calibrations of the mathematical model were then implemented, leading to a high level of confidence with the empirical data obtained, thereby leading to a successful system qualification for the flight campaign.
Rocznik
Strony
16--27
Opis fizyczny
Bibliogr. 14 poz., fot., rys., wzory
Twórcy
autor
  • Space Technologies Center, Łukasiewicz Research Network - Institute of Aviation, Al. Krakowska 110/114, 02-256 Warsaw, Poland
autor
  • Space Technologies Center, Łukasiewicz Research Network - Institute of Aviation, Al. Krakowska 110/114, 02-256 Warsaw, Poland
  • Space Technologies Center, Łukasiewicz Research Network - Institute of Aviation, Al. Krakowska 110/114, 02-256 Warsaw, Poland
Bibliografia
  • [1] NASA Goddard Space Flight Center, Wallops Flight Facility. “NASA Sounding Rockets User Handbook,” 2015.
  • [2] Cieśliński, D., Noga, T., and Pazik, A. “Polish Civil Rockets’ Development Overview.” In: Obronność RP XXI wieku w teorii i praktyce (2021), Dęblin, Wydawnictwo Lotniczej Akademii Wojskowej: pp. 61-102.
  • [3] Nowakowski, P., Pakosz, M., Cieśliński, D., Bartkowiak, B., Wolański, P., and Okniński, A. “Development of Small Solid Rocket Boosters for the ILR-33 Sounding Rocket.” Acta Astronautica Vol. 138 (2017): pp. 374-383. DOI 10.1016/j.actaastro.2017.06.007.
  • [4] Marciniak, B., Okniński, A., Bartkowiak, B., Pakosz, M., Sobczak, K., Florczuk, W., Kaniewski, D., Matyszewski, J., Nowakowski, P., Cieśliński, D., Rarata, G., Surmacz, P., Kublik, D., Rysak, D., Smętek J., and Wolański, P. “Development of the ILR-33 “Amber” Sounding Rocket for Microgravity Experimentation.” Aerospace Science and Technology Vol. 73 (2018): pp. 19-31. DOI 10.1016/j.ast.2017.11.034.
  • [5] Pakosz, M., Noga, T., Kaniewski, D., Okniński, A., and Bartkowiak, B. “24th ESA Symposium on European Rocket and Balloon Programmes and Related Research.” In: ILR-33 AMBER Rocket-Quick, Low Cost and Dedicated Access to Suborbital Flights for Small Experiments. Essen, 2019.
  • [6] Pakosz, M., Matysek, K., Nowakowski, P., Noga, T., Majewska, E., and Ptasiński, G. “Design Modifications for Performance Enhancement of a Suborbital Rocket ILR-33 AMBER 2K.” In: 71st International Astronautical Congress (IAC) - The Cyber Space Edition. International Astronautical Federation (IAF), 2020.
  • [7] Meakin, R.L. “Unsteady Aerodynamic Simulation of Multiple Bodies in Relative Motion: A Prototype Method.” American Institute of Aeronautics and Astronautics, NASA Technical Memorandum 102181, 1989.
  • [8] Lochan, R., Adimurthy, V., and Kumar, K. “Separation Dynamics of Strap-On Boosters.” Journal of Guidance, Control and Dynamics Vol. 15 No. 1 (1992): pp. 137-143. DOI 10.2514/3.20811.
  • [9] Lochan, R., Adimurthy, V., and Kumar, K. “Separation Dynamics of Strap-On Boosters in the Atmosphere.” Journal of Guidance, Control and Dynamics Vol. 20 No. 4 (1997): pp. 633-639. DOI 10.2514/2.4110.
  • [10] Seongjin, C., Soon-Heum, K., Chongam, K., Oh-Hyun, R., and Jeong-Joo, P. “Numerical Analysis on Separation Dynamics of Strap-On Boosters in the Atmosphere.” KSAS International Journal Vol. 2 No. 2 (Nov. 2001): pp. 1-17.
  • [11] AMA Inc., “Aircraft Store Separation and Carriage Loads Analysis: STRLNCH.” [Online]. Available at: https://www.ama-inc.com/strlnch. (accessed on 7 September 2022).
  • [12] Krzysiak, A., Cieśliński, D., Placek, R., and Kekus, P. “Experimental Study of the Boosters Impact on the Rocket Aerodynamic Characteristics.” Aircraft Engineering and Aerospace Technology Vol. 95 No. 2, (2022): pp. 193-200. DOI 10.1108/AEAT-01-2022-0025.
  • [13] Ruchała, P., Placek, R., Stryczniewicz, W., Matyszewski, J., Cieśliński, D., and Bartkowiak, B. “Wind tunel Tests of Influence of Boosters and Fins on Aerodynamic Characteristics of the Experimental Rocket Platform.” Transactions of the Institute of Aviation No. 4(249) (2017): pp. 82-102. DOI 10.2478/tar-2017-0030.
  • [14] Łukasiewicz Research Network - Institute of Aviation. “Pierwsze testy poligonowe rakiety BURSZTYN w wersji 2K i mobilnej wyrzutni rakietowej WR-2.” [Online]. Available at: https://ilot.lukasiewicz.gov.pl/pierwsze-testy-poligonowe-rakiety-bursztyn-w-wersji-2k-i-mobilnej-wyrzutni-rakietowej-wr-2/. (accessed on 15 May 2023).
Uwagi
Opracowanie rekordu ze środków MNiSW, umowa nr SONP/SP/546092/2022 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2024).
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-dfc2ce88-4ed7-4c46-a1e3-aff5fc5fea6f
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