Satellite Thermal Cutter
Description
The clamping and release mechanism uses a thermal cutter and separable nut to achieve high-reliability clamping and separation of spacecraft and solar arrays. This mechanism features no pyrotechnics, low impact, compact size, light weight, and can be reused on the ground. It is widely used for locking and on-orbit release of solar arrays, antennas, and other space structures on satellites.
Parameters:
| Weight | 92±3g |
| Dimensions (mm) | 63 x 58.5 x 17 |
| Unlocking Time | ＜7s |
| Clamping Force | ≥1500N |
| Reliability | Not less than 0.9999 |
| Power Consumption | 4W |
| Operating Temperature | -80℃ to +80℃ |
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contact us
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Dubai headquarters
Address：
Units 610 & 611, Level 3, The Offices 3, One Central Dubai World Trade Centre, Dubai
Phone：
(+971) 04 594 3961
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Hong Kong headquarters
Address：
15/F, Data Technology Hub, 5 Chun Cheong Street, Tseung Kwan O Industrial Estate, New Territories, Hong Kong
Phone：
(+852) 2161 8300
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E-mail
ir@uspace.com
