A paste-propellant rocket propulsion system

1Ivanchenko, AM
1Yangel Yuzhnoye State Design Office, Dnipropetrovsk, Ukraine
Kosm. nauka tehnol. 1999, 5 ;(4):03-10
https://doi.org/10.15407/knit1999.04.003
Section: Space-Rocket Vehicles
Publication Language: Ukrainian
Abstract: 
The effort in constructing a paste-propellant rocket propulsion system in Ukraine is described. Construction features for keeping flame from penetrating to the fuel supply system and maintaining combustion are considered. A formula is proposed for calculating the consumption of the propelland which moves through a spinneret with a conical ring-type slot. The paste-propellant rocket propulsion system is shown theoretically as well as experimentally to be more efficient in the thrust control as compared to other rocket propulsion systems.
Keywords: paste-propellant, rocket propulsion system, thrust control
References: 
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3. Griffin W. S., Mann R. W., Marston Ch. H. Solid propellant burning control systems: Patent US 3266247 A (1966).

4. Khan Ch. D. Rheology in Processing of Polymers, 110—129 (Khimiya, Moscow, 1971) [in Russian].