NOZZLE-FREE SOLID-PROPELLANT ROCKET ENGINE Russian patent published in 2014 - IPC F02K9/12 

Abstract RU 2517971 C1

FIELD: engines and pumps.

SUBSTANCE: proposed engine comprises combustion chamber with front bottom, cylindrical part and rear end and charge with central channel secured to combustion chamber. Said charge consists of two tandem parts. Charge larger part is located nearby bottom and has cylindrical central channel. Charge smaller part is located nearby combustion chamber rear end and has the central channel. Central channel flow section area increases smoothly toward outlet cross-section and is made from fuel with combustion rate some 30÷50% smaller than that of the charge larger part. Smaller charge weight makes 2÷10% of the charge total weight.

EFFECT: higher efficiency of solid-propellant charge.

5 cl, 2 dwg

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RU 2 517 971 C1

Authors

Gubertov Arnol'D Mikhajlovich

Mironov Vadim Vsevolodovich

Davydenko Nikolaj Andreevich

Borisov Dmitrij Marianovich

Ul'Janova Marina Viktorovna

Degtjarev Sergej Antonovich

Dates

2014-06-10Published

2012-12-29Filed