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Mekanisma fisarahana amin'ny satelita-rocket

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Satellite-Rocket Separation Mechanism

Mekanisma fisarahana amin'ny satelita-rocket

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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Description

Product Detail

 

 

Code Product

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

lanja

1.2kg

1.8kg

3.3kg

Ny fonon'ny tena

220×220×81mm

270×270×84mm

390×390×85mm

Temperature Range

-70~+70 ℃

Mamaha ny Impact

<600g (domaine matetika)

Cycle famatsiana

3 volana

 

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Reliable Satellite-Rocket Separation Mechanism

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