Trident II first and second stage internal insulation

Power plants – Reaction motor – Solid propellant

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Details

60255, 264236, 264314, F02K 900, B29C 7100

Patent

active

047110864

ABSTRACT:
A rocket motor insulator of varied thickness with an integrated flap to rce propellant stresses.

REFERENCES:
patent: 3080269 (1963-03-01), Pollock et al.
patent: 3937781 (1976-02-01), Allen
patent: 3946557 (1976-03-01), Macbeth
patent: 3962865 (1976-06-01), McCone, Jr.
patent: 3965676 (1976-06-01), Schaffling
patent: 4031154 (1976-12-01), O'Driscoll
patent: 4085584 (1978-04-01), Jones et al.
patent: 4118928 (1978-10-01), Lyles
patent: 4187676 (1980-02-01), O'Neil et al.
patent: 4458483 (1984-07-01), Vetter

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