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