Thrust nozzle with insulation

Power plants – Reaction motor – With thrust direction modifying means

Patent

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Details

60242, 60253, 23926543, F02K 100

Patent

active

046497013

ABSTRACT:
A thrust nozzle of the hollow-cone type affixed to a stationary shell having external insulation on the nozzle and the shell and the nozzle having a liner extending beyond its edge and having insulation over the extended portion.

REFERENCES:
patent: 3446437 (1969-05-01), McCullough
patent: 3572029 (1971-03-01), Swit, Jr.
patent: 3696999 (1972-10-01), Desjardins
patent: 3698192 (1972-10-01), Le Febvre, Jr.
patent: 3726480 (1973-04-01), Miltenberger
patent: 3936058 (1976-02-01), Clark et al.
patent: 3946557 (1976-03-01), MacBeth
patent: 4180211 (1979-12-01), Olcott et al.
patent: 4441312 (1984-04-01), Smith
patent: 4489889 (1984-12-01), Inman
Wilson et al., Dual Flex-A Low Horsepower Flexible Seal Nozzle, J. Spacect + Rockets, vol. 9, No 8, Aug., 1972, pp. 567+8.

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