DESIGNING A RAPID GAS-GENERATOR FOR A SPECIFIED CONSUMABLES CHARACTERISTIC
In article one of methods of increase in range of aircraft due to use of the rocket straight-flow engines is considered. The technique of design of a charge of a gas generator of RSFE is given. Merits and demerits of this type of the engine are considered and also requirements to fuel are formulated. The mathematical model allowing to model process of work of a gasgenerator for obtaining the set account characteristic is presented.