• GaInP/GaAs/Ge or Silicon
Photovoltaics • Carbon Fiber Structures • Structural or Cable Synchronized • Deployment with
Non-Pyrotechnic Release • Provides Stowed Power • Long or Transverse Axis Deployment • 1/2 kW to 6 kW Power • 25 W/kg to 65 W/kg • High Stiffness (0.3 Hz to 0.7 Hz) • Mass Moment of Inertia (~300 kg-m2) | • Low-Risk Heritage Technology • Simple, Easily Adaptable
Spacecraft Interfaces • Low Non-Recurring Engineering • Flight Heritage Components and Processes • 11-16 Month Delivery Time • Streamlined Spacecraft Integration 
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