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Title:
SELF-PROPELLED MISSILE LAUNCHER
Document Type and Number:
Japanese Patent JP2017007400
Kind Code:
A
Abstract:
PROBLEM TO BE SOLVED: To provide a self-propelled missile launcher capable of stabilizing a vehicle body during launch of a missile and, at the same time, supporting a vehicle body rear part while permitting movement of a vehicle during re-loading of a missile without entailing increases in the number of components and weight and complication of a structure.SOLUTION: A roller-added support leg 31, which includes a roller 33 provided in a skeleton member 32 extending downward from a rear end portion of a vehicle body frame 10 and connecting to ground while permitting movement of a vehicle 2 in a longitudinal direction during a loading operation for re-loading a cargo box 3 and an unloading operation; and a ground contact leg 34 provided in the skeleton member 32, extending downward of the roller 33 during launch of a missile to connect to the ground, and restricting the movement of the vehicle, is provided in the rear end portion of the vehicle body frame 10.SELECTED DRAWING: Figure 1

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Inventors:
OZAKI YASUTAKA
Application Number:
JP2015121981A
Publication Date:
January 12, 2017
Filing Date:
June 17, 2015
Export Citation:
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Assignee:
IHI AEROSPACE CO LTD
International Classes:
B60P1/48; B60P3/00; B60S9/12; F41F3/042
Domestic Patent References:
JP2006153302A2006-06-15
JP2008012968A2008-01-24
JP2006341990A2006-12-21
JPS6011864U1985-01-26
JPH08318834A1996-12-03
JPS61117038U1986-07-24
Foreign References:
US20100236391A12010-09-23
Attorney, Agent or Firm:
Koji Nagato