Strength |
Ø Inherited from DFH-4 series Ø Minimized project CAPEX and time-to-market risk Ø Compatible with low-cost launch vehicles Ø Auto operation during LEOP and in orbit |
Capability |
Ø Satellite: 1800~2100kg / 8~10kW Ø Payload: 300~450kg / 3~4kW Ø Lifetime: 15 years Ø Propulsion: All-Electric Propulsion |
Application |
Ø To be launched, several in contract negotiation phase Ø Ideal for business trial and expansion with limited capital, demand or F&O |