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Satellite-Rocket Separation Mechanism
The satellite-rocket separation mechanism adopts the non-initiating explosive separating nut to realize a high degree of stiffness and reliable locking. The disengaging spring is adopted to conduct pushing-type separation of the unlocked satellite, with the features of the stable separation posture, simple mechanical interface, etc., and it is suitable for low-impact unlocking and separation of 100-kilogram small sa…
SupplierAstralink Science and Technology Co., Ltd.www.space-navi.com
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Products Detail
Product Code | SC-CA-SRSM-102-01-5~15kg | SC-CA-SRSM-102-02-15~40kg | SC-CA-SRSM-102-03-40~80kg |
Applicable Satellite Load | 5~15kg | 15~40kg | 40~80kg |
Separation Angular Velocity | <5°/s | <4°/s | <2.5°/s |
Separation Velocity | 0.4~0.6m/s | 0.4~0.6m/s | 0.4~0.6m/s |
Weight | 1.2kg | 1.8kg | 3.3kg |
Main Body Envelopment | 220×220×81mm | 270×270×84mm | 390×390×85mm |
Temperature Range | -70~+70℃ | ||
Unlocking Impact | <600g (frequency domain) | ||
Supply Cycle | 3 months | ||
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Astralink Science and Technology Co., Ltd.
