HYBRID PROPELLANT ROCKET MOTOR | ||||
| International Conference on Aerospace Sciences and Aviation Technology | ||||
| Article 14, Volume 8, ASAT Conference, 4-6 May 1999, May 1999, Page 1-15 PDF (2.02 MB) | ||||
| Document Type: Original Article | ||||
| DOI: 10.21608/asat.1999.24884 | ||||
 View on SCiNiTO | ||||
| Author | ||||
| Frantitek LUDVIK | ||||
| Prof. Dipl.Eng., Ph.D., Department of Rocketry, Military Academy in Brno, Czech Republic. | ||||
| Abstract | ||||
| The paper deals with hybrid propellant rocket motor as a propulsion unit of prospective rocket weapon systems, as well as a drive unit of some cosmic rocket carriers. There are introduced possible constructional schemes of hybrid propellant rocket motor and is mentioned further on the particular general internal ballistic solution of the solid part of the hybrid propellant. The paper shows the advantages and disadvantages of such types of propulsion units. | ||||
| Keywords | ||||
| Hybrid propulsion; hybrid rocket; Internal Ballistics; Rocket motor | ||||
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