FIELD: space technology.
SUBSTANCE: group of inventions relates to space technology. Disclosed is an ejector for at least one satellite, in particular a picosatellite, having a body, a fixing device for holding the satellite. The fixing device has a lid for covering the inner space. The lid can be blocked in the closed position by means of at least one sliding bolt releasably relative to the body. The release mechanism has a slider connected to the bolt, provides movement of the bolt from the locking position to the disengaged position. In this case, the slider is held under preload in the blocking position and is released from this position.
EFFECT: group of inventions ensures reliable fixation of the satellite in the ejector during transportation to the place of ejection.
24 cl, 15 dwg
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|
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|
RU2611322C1 |
Authors
Dates
2021-03-17—Published
2017-05-04—Filed