CHOOSING THE DESIGN APPROACH AT ELECTRICAL POWER SUPPLY SYSTEM DEVELOPMENT FOR HYPERSONIC AIRCRAFT

The specific peculiarities of design of electrical power supply system for hypersonic aircraft and issues of the decision choice on key design objectives are considered. It is shown that the most difficult design goals of electrical power supply system for hypersonic aircraft relate to the choice of the accumulator battery type and ensuring effective power supply of airplane systems. Also this paper deals with the solutions of problems of the battery type choice, structural synthesis and conditions of ensuring the target level of energy efficiency at maintenance of necessary thermophysical properties.