MULTI-FUNCTIONAL STRUCTURE OF LOAD-BEARING ENVELOPE OF PRESSURE-TIGHT COMPARTMENT OF SPACECRAFT

摘要

space engineering. SUBSTANCE: load- bearing envelope includes inner pressure-tight envelope and external non- pressure-tight envelope which are connected by means of glass honeycomb members whose cells are filled with packs of shield-vacuum heat insulation. EFFECT: reduced mass of spacecraft at extended service life; enhanced resistance to action of high-velocity natural and artificial particles. 3 dwg