On the implementation of potential energetic characteristics of composite solid propellants for cruise solid fuel engines of ballistic rockets under strict limitations for sixes and boost path durations

S. A. Bitkin<sup>ab

a</sup> South Ural State University, Miass Branch, Miass, Chelyabinsk Region, Russia
^b Joint Stock Company «Academician V.P. Makeyev State Rocket Centre», Miass, Chelyabinsk Region, Russia;

Abstract: The implementation directions of potential energetic characteristics of composite solid propellants for cruise solid fuel engines of ballistic rockets have been considered. The effects of nozzle size, combustion chamber pressure and duration of engine's run have been shown.

Keywords: energetic characteristic, composite solid propellant, design parameter, solid fuel rocket engine, optimization.

UDC: 621.454.3