Structural external insulation for hypersonic missiles

Details Structural external insulation for hypersonic missiles Structural external insulation for hypersonic missiles

1985-12-16

1987-11-17

Nase, Jeffrey V.

Aeronautics and astronautics

Spacecraft

Spacecraft formation, orbit, or interplanetary path

4284735, 523179, 523138, B64G 158

Patent

active

047069120

ABSTRACT:
A structural external insulation for hypersonic missiles which reach speeds hat cause surface temperatures on the cylindrical shell structure to reach up to 3000.degree. F. for a period of time. The invention incorporates efficient high temperature insulation as an integral part of the composite shell manufacturing process (tape layup and/or filament winding).

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