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  • Low-Cost Solid Rocket Motor Development

    Paper number

    IAC-14,C4,P,52,x24179

    Author

    Mr. Adam Okninski, Institute of Aviation, Poland

    Coauthor

    Mr. Bartosz Bartkowiak, Warsaw University of Technology, Poland

    Coauthor

    Mr. Pawel Nowakowski, Warsaw University of Technology, Poland

    Coauthor

    Ms. Joanna Zaborowska, Warsaw University of Technology, Poland

    Coauthor

    Mr. Damian Kaniewski, Warsaw University of Technology, Poland

    Coauthor

    Mr. Blazej Marciniak, Warsaw University of Technology, Poland

    Coauthor

    Mr. Jan Matyszewski, Warsaw University of Technology, Poland

    Coauthor

    Dr. Jan Kindracki, Warsaw University of Technology, Poland

    Coauthor

    Prof. Piotr Wolanski, Polish Academy of Sciences, Poland

    Year

    2014

    Abstract
    This paper gives an overview of the development of solid rocket motors of the Polish Small Sounding Rocket Program. The team efforts enabled manufacturing of high performance rocket motors using low-cost, mainly off-the–shelf, technologies. This paper presents the design and optimization methodologies. A description of software developed during the project is contained. Structural and interior ballistics optimization techniques are described. Optimization focused on adapting the rocket thrust curve to specific mission requirements is also discussed. Technical equipment and background is presented. This paper introduces a technology of producing low-cost composite structure solid propellant rocket motors without expensive filament winding  machinery. All of the main parts of the motors are presented. Performance simulations and firing results of sub-scale rocket motors of thrusts between 500 and 5000 Newtons are given. Flight operation data is also presented and analyzed. Finally, a detailed comparison of similar size rocket motors is shown, proving an efficient and economic design. The ultimate aim is to build larger rocket motors enabling intensive suborbital experimentation and preparing the developed design for launcher operation. This work is based on results of the joint project of the Space Technology Department of the Institute of Aviation and the Division of Aircraft Engines of the Institute of Heat Engineering of Warsaw University of Technology (WUT) with a key role played by members of the Students’ Rocketry Group of the WUT Students’ Space Association.
    Abstract document

    IAC-14,C4,P,52,x24179.brief.pdf

    Manuscript document

    (absent)