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.
LUDVIK, F. (1999). HYBRID PROPELLANT ROCKET MOTOR. International Conference on Aerospace Sciences and Aviation Technology, 8(ASAT Conference, 4-6 May 1999), 1-15. doi: 10.21608/asat.1999.24884
MLA
Frantitek LUDVIK. "HYBRID PROPELLANT ROCKET MOTOR", International Conference on Aerospace Sciences and Aviation Technology, 8, ASAT Conference, 4-6 May 1999, 1999, 1-15. doi: 10.21608/asat.1999.24884
HARVARD
LUDVIK, F. (1999). 'HYBRID PROPELLANT ROCKET MOTOR', International Conference on Aerospace Sciences and Aviation Technology, 8(ASAT Conference, 4-6 May 1999), pp. 1-15. doi: 10.21608/asat.1999.24884
VANCOUVER
LUDVIK, F. HYBRID PROPELLANT ROCKET MOTOR. International Conference on Aerospace Sciences and Aviation Technology, 1999; 8(ASAT Conference, 4-6 May 1999): 1-15. doi: 10.21608/asat.1999.24884
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