Lateral support system for canister-launched missile

Ordnance – Rocket launching – Having tubular guide means

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Details

277216, F41F 304, F16J 1510

Patent

active

044649720

ABSTRACT:
A novel lateral support system for a canister launched missile is provided which comprises, a plurality of long, narrow flexible pads of elastomer or like material disposed on the surface of said missile along a substantial lengthwise portion thereof and configured to substantially fill the annular gap between the missile and canister, each of said pads being hingedly attached near the canister exit opening whereby the pads are peeled from the surface of the missile during launch thereof.

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