FIELD: astronautics.
SUBSTANCE: invention relates to means of soft vertical landing, mainly of space object. In the system of deployment of landing supports (LS) there are used drive mechanisms: extension supports and devices for extension of telescopic rods of LS, as well as devices for separation LS - pneumatic type. Said mechanisms and devices are connected via pipelines with filling and electric pneumatic valves and via pneumatic collectors to high-pressure cylinders of pneumatic unit. Said extendable stops and extension devices are equipped with contact transducers and extension sensors connected with control unit, respectively. This unit controls the operation of the system at LS separation, their turning and extension of the LS rods to the working position during landing.
EFFECT: technical result of invention is multiple disclosure of LS.
1 cl, 2 dwg
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Authors
Dates
2020-06-29—Published
2019-03-04—Filed