Lateral support device system for canister-launched missile
AssigneeAgency for Defense Development
InventorsIl-Soo Kim, Woo-Jeon Shim, Hak-Yeol Lee
Life of this patent
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Abstract
A lateral support device system of a canister-launched missile of the present invention is provided for eliminating the clearances between missile and the canister in 4 places by 90 degrees interval, and therefore no relative movement occurs between the missile and the canister. Therefore, the missile and the detent is free from shocks and vibrations that occurs during the handling, transportation and operation. In addition, when the missile is fired, those lateral lock become free with a little energy loss.
Claims8
A lateral support device system for a canister-launched missile comprising:
- sabots formed on an outer circumferential surface of a missile;
- a travel lock bar which is integrally fixed to the each sabot;
- and
- a travel lock bolt fixed at the canister and selectively pressing the upper end of the travel lock bar so as to be contact with the travel locking bar.
A lateral support device system for a canister-launched missile comprising:
- sabots formed on an outer circumferential surface of a missile;
- and
- a travel lock bolt fixed at the canister and selectively pressing the upper surface of the each sabot so as to be contact with the sabots.
Dependencies are inferred from the claim text.