TLF:+86 13943095588
dansk

Satellit-raketadskillelsesmekanisme

hjem > Produkter >Komponent >Satellitkomponenter > Satellit-raketadskillelsesmekanisme
Satellite-Rocket Separation Mechanism

Satellit-raketadskillelsesmekanisme

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.

Dele:
Kontakt os nu > Download
BESKRIVELSE

Produktdetaljer

 

 

Produktkode

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

Vægt

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)

Forsyningscyklus

3 måneder

 

We are interested in your Satellite-Rocket Separation Mechanism.

Please provide technical specifications and pricing.

Kontakt os

Reliable Satellite-Rocket Separation Mechanism

Relaterede produkter
tilbage |næste
Relaterede nyheder
tilbage |næste

Hvis du er interesseret i vores produkter, kan du vælge at efterlade dine oplysninger her, så kontakter vi dig snarest.


Tryk på Enter for at søge eller ESC for at lukke