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
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.