סאַטעליט-ראַקעט סעפּאַראַטיאָן מעקאַניזאַם

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.

ייַנטיילן:

קאָנטאַקט אונדז איצט > אראפקאפיע

באַשרייַבונג

פּראָדוקטן דעטאַל

פּראָדוקט קאָד	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
וואָג	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)
צושטעלן ציקל	3 חדשים