The method of investigation of basic project parameters of microsatellite by random search

Abstract

A significant number of the main design parameters of the small upper stage for the group launch of small spacecraft with a propulsion system with a displacement fuel supply system determines the relevance of the random search method. The aim of the work is to create a method of selecting the main design parameters of the small upper stage by random search. The mathematical model based on the dimensional-mass model of the calculated mass determination provides the choice of the optimal mass of the upper stage, taking into account the complex relationships of the studied parameters

Keywords

• adapter
• small spacecraft
• small upper stage
• basic design parameters
• random search method