Hybrid rocket engines: The benefits and prospects |
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| Institution: | 1. Department of Chemistry, Royal Military Academy, Avenue de la Renaissance 30, 1000 Brussels, Belgium;2. Faculty of Gama, University of Brasília, Área Especial de Indústria e Projeção A, 72444-240 Brasília, Brazil;3. Aero-Thermo-Mechanics department, Université Libre de Bruxelles, F.D. Roosevelt Avenue 50, 1050 Brussels, Belgium;1. ONERA - The French Aerospace Lab, F-31410, Mauzac, France;2. DELTACAT Ltd, Kintyre House, 70 High Street, Fareham, Hampshire, PO16 7BB, UK;3. Aeronautics and Astronautics Unit, University of Southampton, UK;4. Airbus Defence and Space, F-31400 Toulouse, France;1. School of Astronautics, Beihang University, Beijing 100191, China;2. China Academy of Launch Vehicle Technology, Beijing 100076, China;1. School of Astronautics, Beihang University, Beijing, China;2. Science and Technology on Space Physics Laboratory, China Academy of Launch Vehicle Technology, Beijing, China;3. Beijing Institute of Electronic System Engineering, Beijing, China;4. Systems Engineering Division, China Academy of Launch Vehicle Technology, Beijing, China |
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| Abstract: | The review of research avenues for working processes (ignition, combustion, etc.) in hybrid rocket engines (HRE), for thermal protection and power characteristics is stated. Based on conducted design and exploratory studies and design developments, the reasonable fields of application of HRE to launch systems for orbit insertion of payload are determined. |
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