固体火箭发动机内孔星形药柱采用J^＊准则时在不同条件下的解析设计

ANALYTICAL DESIGN BASED ON PRINCIPLE J* FOR INTER-NAL BURNING STAR GRAINS OF SOLID ROCKETSUNDER DIFFERENT CONDITIONS

This paper is the systematic development of 2] and 3] . Based on the printiple J* of the limitation of scouring combustion, we have established more perfect design cquation series. The combination of design equations and the computer programs under different tactical requirements have also been given in this paper. Thus it makes the analytical design shown in my original works of 2] and 3] to have universal applicability and completeness.