Title:
FLIGHT VEHICLE LAUNCHER
Document Type and Number:
Japanese Patent JP3903343
Kind Code:
B2
Abstract:
PROBLEM TO BE SOLVED: To provide a flight vehicle launcher capable of being repeatedly used at low launching cost with a simple structure.
SOLUTION: This flight vehicle launcher 1 has at least a spring means 10 obtained by connecting a compression spring 12 and a tension spring 13 in series through a cradle 11, an engaging means 30 formed on the cradle 11 and engaged with the flight vehicle 2, a tensing means 40 for moving the cradle 11 in one direction to simultaneously achieve the compression of the compression spring 12 and the tension of the tension spring 13, and a latching means 70 for positioning and supporting the cradle 11 tensed in one direction by the tensing means 40. The latching by the latching means 70 is released, whereby the compressed compression spring and the tensed tension spring are simultaneously released to move the cradle 11 and to launch the flight vehicle 2.
Inventors:
Yuichi Mimi
Application Number:
JP2003275399A
Publication Date:
April 11, 2007
Filing Date:
July 16, 2003
Export Citation:
Assignee:
Yuichi Mimi
International Classes:
F41F7/00; A63H27/14; B64F1/04; (IPC1-7): F41F7/00; A63H27/14; B64F1/04
Domestic Patent References:
| JP52130733A | ||||
| JP58070298U |
Attorney, Agent or Firm:
Takahisa Kimura
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