FIELD: rocket and small-arms armament testing systems.
SUBSTANCE: the rig has a fixed platform, movable carriage with a launching device fastened on it, and a transducer for monitoring the characteristic of linear motion of the carriage. The movable carriage is positioned on rectilinear horizontal guides by means of the upper and lower roller supports, the guides are rigidly fastened on the fixed platform and provided on two sides with carriage motion stops. The transducer for monitoring the characteristic of the carriage linear motion is made in the form of a permanent magnet fastened on the carriage, and a strip-insulator with a current-conducting winding installed opposite it.
EFFECT: provided adjustment of the value and direction of the momentum by a purposeful variation of the construction of the launching device or rocket.
3 dwg
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Authors
Dates
2006-10-10—Published
2005-02-10—Filed