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Satellite-Rocket Separation Mechanism

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Satellite-Rocket Separation Mechanism

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 satellites.

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Produkten Detail

 

 

Produkt 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

Gewicht

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 moanne

 

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