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