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GROUND FIRE TESTING DEVICE AND METHOD FOR THRUST MEASUREMENT OF SOLID ROCKET MOTOR USING CANTED NOZZLE
GROUND FIRE TESTING DEVICE AND METHOD FOR THRUST MEASUREMENT OF SOLID ROCKET MOTOR USING CANTED NOZZLE
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机译:倾斜喷嘴用于实心火箭发动机推力测量的地火测试装置及方法
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摘要
The present invention relates to an apparatus for a ground combustion test for measuring thrust of a solid thruster using an inclined nozzle. The present invention comprises: a ground combustion test tool formed to cover a motor of the solid thruster to be fastened to the ground combustion test apparatus; an adapter connection bar for connecting the ground combustion test tool to a load cell for measuring thrust; and a three-axis supporter installed perpendicular to a central shaft of the load cell to fix the ground combustion test tool to the ground combustion test apparatus. Therefore, the ground combustion test can be performed by allowing a central shaft of the inclined nozzle to coincide with the central shaft of the load cell.
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