A
spacecraft adjustable locking and releasing mechanism includes a shaft
system, a pin puller locking sleeve, a pyrotechnic pin puller, an adjusting
assembly, a pin puller pressing sleeve and a base; the relative position between the pyrotechnic pin puller and the shaft
system can be adjusted by the adjusting
assembly, and the pyrotechnic pin puller presses against the shaft
system after the adjusting
assembly applies a specified preload, thereby realizing the locking function of the
spacecraft launch section; the adjusting assembly is rotated in the opposite direction to realize the manual unlocking function on the ground; after the
spacecraft enters
orbit, the pin puller igniter is detonated, and the high-temperature and high-pressure gas generated pushes the pin puller
piston to move, overcoming the
friction force while
cutting off the locking pin, and the
piston retracts into the pin puller body, thereby realizing the function of releasing the shaft system. The present invention can lock when the shaft system is in an orthogonal retracted state, reducing the overall range envelope of the spacecraft, which is conducive to the
spacecraft system to coordinate the position planning of each single
machine; the unlocking and releasing function relies on the pyrotechnic pin puller to
cut off the locking pin, does not rely on other auxiliary parts, and has a high degree of reliability.