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On the issue of selecting burned materials in rocket vehicle designs
Author(s) -
V. I. Trushlyakov,
К. И. Жариков
Publication year - 2021
Publication title -
journal of physics. conference series
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.21
H-Index - 85
eISSN - 1742-6596
pISSN - 1742-6588
DOI - 10.1088/1742-6596/1791/1/012029
Subject(s) - rocket (weapon) , property (philosophy) , incineration , production (economics) , aerospace engineering , construction engineering , engineering , computer science , forensic engineering , mechanical engineering , waste management , philosophy , epistemology , economics , macroeconomics
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.

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