A controllable self-protection small tether ejection release mechanism
A release mechanism and self-protection technology, which is applied in the field of space tethered satellite systems to achieve effective smooth control and improved reliability
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[0031] The present invention will be further explained below in conjunction with the accompanying drawings.
[0032] like figure 1 As shown, the present invention provides a controllable self-protection small tethered ejection release mechanism, including a satellite simulator 45, an ejection separation module, a tether cutting module, a tension control module, a spool base module and a base platform;
[0033] The satellite simulator 45 is provided with a guide cone 46, which is connected to the ejection separation module; the guide cone 46 includes an electromagnet. The spool base module extends out of the tether 44 to connect with the satellite simulator 45 . The tether 44 is preferably a Dyneema tether, which melts instantly when it hits the heating wire and can be more effective than conventional shearing
[0034] The ejection separation module is as Figure 2-3 As shown, it includes a butt cone 1, a damping rubber 2, a first fixing piece 3, a toothless gear 4, a first ...
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