Method and apparatus for stabilizing the in-tube trajectory of a

Details Method and apparatus for stabilizing the in-tube trajectory of a Method and apparatus for stabilizing the in-tube trajectory of a

1984-06-19

1995-08-08

Jordan, Charles T.

Ordnance

Rocket launching

Having tubular guide means

89 181, F41F 304

Patent

active

054389054

ABSTRACT:
Apparatus and method for bypassing eject gas around an annular seal disposed between the trailing end of a missile and a launch tube only in an area where the trailing end of the missile is close to the launch tube in order to provide a centering force on the trailing end of the missile to stabilize the in-tube trajectory of the missile during ejection.

REFERENCES:
patent: 3100421 (1963-08-01), Moy
patent: 3124040 (1964-03-01), Fieldler
patent: 3166978 (1965-01-01), Price et al.
patent: 3266373 (1966-08-01), Brown
patent: 3289533 (1966-12-01), Brown
patent: 3857321 (1974-12-01), Cohen
patent: 4357855 (1982-11-01), Merz
patent: 4399999 (1983-08-01), Wald
patent: 4406211 (1983-09-01), Andersen
patent: 4433848 (1984-02-01), Williams
patent: 4464972 (1984-08-01), Simon
patent: 5315912 (1994-05-01), Huber et al.

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