Internal umbilical connector for missiles

Details Internal umbilical connector for missiles Internal umbilical connector for missiles

1976-09-01

1977-06-28

Brown, David H.

Ordnance

Rocket launching

Having umbilical-separating means

102105, 244 31, F41F 304

Patent

active

040318060

ABSTRACT:
An assembly which is an energy absorbing system for supporting the nose c of a missile in a position extended from the guidance section prior to eject (launch) of the missile. This extended position exposes internal umbilical connectors to permit internal missile components to be connected to external sources of power (electrical, pneumatic, etc.). Gravitational forces during eject (launch) displace the nose cone rearwardly against the guidance section. The assembly controls impact velocity of the nose cone and guidance section during closure thereof. At closure, a smooth aerodynamic surface is formed at the junction of the nose cone and guidance section.

REFERENCES:
patent: 2814250 (1957-11-01), Everett
patent: 2936710 (1960-05-01), Bollay
patent: 3152667 (1964-10-01), Powell
patent: 3262655 (1966-07-01), Gillespie
patent: 3444779 (1969-05-01), Buell et al.
patent: 3490373 (1970-01-01), Fox

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