Author:
Trushlyakov V I,Zharikov K I
Abstract
Abstract
The concept of selecting materials for the design of separable parts of missiles with a property that ensures their rapid disposal by burning after the mission is completed is considered. The characteristics of incinerated materials are presented. The choice of materials based on the proximity of thermal and strength characteristics to existing structural materials used in the production of traditional head fairings is made.
Subject
General Physics and Astronomy