FIELD: space technology.
SUBSTANCE: invention relates to the field of space technology, more specifically to separation systems. A payload reset system contains a holding device, detachable using a pyrolock, including mechanical locks located on a frame of a supporting structure, and a piston. Each of locks contains a rod and a holding link. The lock rod passes through a hole made in a payload frame, and it is equipped with a spring. The pyrolock is made in the form of a case mounted in the frame of the supporting structure and fixed by protrusions from movement in the direction of the longitudinal axis. The pyrolock case has a lever equipped with an axis mounted in an oval cutout of a disc. The piston enclosing the case, partially immersed to a reciprocal cutout on the payload frame, is equipped with sliding rollers. Membrane is mounted in the piston, which, at the end section of the piston movement, is cut by a knife mounted in the payload frame.
EFFECT: increase in the reliability is achieved.
1 cl, 10 dwg
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Authors
Dates
2022-05-13—Published
2021-09-22—Filed