The satellite-rocket separation mechanism adopts non-pyrotechnic separating nut to realize a high stiffness and reliable locking, adopts separating spring to push off the unlocked satellite, with the features of stable separation attitude, simple mechanical interface, etc., and it is suitable for low-shock release and separation of 100-kilogram small satellites.
Product Code | CG-JG-SM-10 | CG-JG-SM-20 | CG-JG-SM-60 |
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℃ |
Release shock | <600g (frequency domain) |
Supply Cycle | 3 months |
