Title:
THREE-AXIS OSCILLATING TYPE ROCKET TEST STAND
Document Type and Number:
Japanese Patent JP3189173
Kind Code:
B
Abstract:
PURPOSE: To provide a three-axis oscillating type rocket test stand capable of confirming-evaluating the safety of an airframe immediately after launching, taking account of disturbance caused by the rolling of a marine vessel or the like at the vertical launching time of a rocket.
CONSTITUTION: A three-axis oscillating type rocket test stand 1 provided with a rocket rotating base rotatable in triaxial directions is provided with actuator mechanism 23 for giving disturbance at the launching time of a rocket with a thrust direction control device, and a release connector 25 capable of separating the rocket from the actuator 23 in correspondence with the ignition timing of the rocket.
Inventors:
Matsumoto, Shinsuke
Takagi, Yasutada
Takagi, Yasutada
Application Number:
JP1992000221049
Publication Date:
May 18, 2001
Filing Date:
August 20, 1992
Export Citation:
Assignee:
TECH RES & DEV INST OF JAPAN DEF AGENCY
NISSAN MOTOR CO LTD
NISSAN MOTOR CO LTD
International Classes:
B64G5/00; B64F5/00; B64G7/00; F42B15/00; F42B35/00; B64G5/00; B64F5/00; B64G7/00; F42B15/00; F42B35/00; (IPC1-7): B64G5/00; B64G7/00; F42B15/00