11 THESE SYSTEM TECHNICAL DRIVERS ALIGN WELL WITH THE INHERENT CAPABILITIES OF OUR HIGH WATTS PER KILOGRAM (HAWK) SOLAR ARRAY THAT HAS COMPLETED QUALIFICATION AND IS AWAITING SPACECRAFT INTEGRATION ON THE AFRL BIARRI MISSION CURRENTLY SCHEDULED FOR LAUNCH IN Q4 2015. WE WILL LEVERAGE SIGNIFICANTLY FROM THE EXISTING HAWK DESIGN AND RISK REDUCTION EFFORTS ALREADY NEARING COMPLETION ON OUR AIR FORCE PROGRAM. OUR PROPOSED SOLAR ARRAY SYSTEM DESIGN MEETS ALL OF THE LISTED REQUIREMENTS. OUR INNOVATIVE APPROACH OFFERS LOWER SYSTEM MASS AND REDUCES OVERALL SYSTEM TECHNICAL RISK. OUR PROPOSED PATENTED THIN PANEL DESIGN IS AN EFFICIENT SOLAR ARRAY STRUCTURE THAT WILL ACHIEVE A SPECIFIC POWER GREATER THAN 140 WATTS/KILOGRAM (W/KG). THE ARRAY PROVIDES OUTWARD FACING CELLS WHEN STOWED SO THAT POWER CAN BE GENERATED BEFORE ARRAY DEPLOYMENT. THE LOW PROFILE PANCAKE GIMBAL SUPPORTS GENERATING MAXIMUM AVERAGE POWER DURING THE MISSION. Other Administrative Action $0 9/7/18 9 THESE SYSTEM TECHNICAL DRIVERS ALIGN WELL WITH THE INHERENT CAPABILITIES OF OUR HIGH WATTS PER KILOGRAM (HAWK) SOLAR ARRAY THAT HAS COMPLETED QUALIFICATION AND IS AWAITING SPACECRAFT INTEGRATION ON THE AFRL BIARRI MISSION CURRENTLY SCHEDULED FOR LAUNCH IN Q4 2015. WE WILL LEVERAGE SIGNIFICANTLY FROM THE EXISTING HAWK DESIGN AND RISK REDUCTION EFFORTS ALREADY NEARING COMPLETION ON OUR AIR FORCE PROGRAM. OUR PROPOSED SOLAR ARRAY SYSTEM DESIGN MEETS ALL OF THE LISTED REQUIREMENTS. OUR INNOVATIVE APPROACH OFFERS LOWER SYSTEM MASS AND REDUCES OVERALL SYSTEM TECHNICAL RISK. OUR PROPOSED PATENTED THIN PANEL DESIGN IS AN EFFICIENT SOLAR ARRAY STRUCTURE THAT WILL ACHIEVE A SPECIFIC POWER GREATER THAN 140 WATTS/KILOGRAM (W/KG). THE ARRAY PROVIDES OUTWARD FACING CELLS WHEN STOWED SO THAT POWER CAN BE GENERATED BEFORE ARRAY DEPLOYMENT. THE LOW PROFILE PANCAKE GIMBAL SUPPORTS GENERATING MAXIMUM AVERAGE POWER DURING THE MISSION. Other Administrative Action $0 6/12/18 10 THESE SYSTEM TECHNICAL DRIVERS ALIGN WELL WITH THE INHERENT CAPABILITIES OF OUR HIGH WATTS PER KILOGRAM (HAWK) SOLAR ARRAY THAT HAS COMPLETED QUALIFICATION AND IS AWAITING SPACECRAFT INTEGRATION ON THE AFRL BIARRI MISSION CURRENTLY SCHEDULED FOR LAUNCH IN Q4 2015. WE WILL LEVERAGE SIGNIFICANTLY FROM THE EXISTING HAWK DESIGN AND RISK REDUCTION EFFORTS ALREADY NEARING COMPLETION ON OUR AIR FORCE PROGRAM. OUR PROPOSED SOLAR ARRAY SYSTEM DESIGN MEETS ALL OF THE LISTED REQUIREMENTS. OUR INNOVATIVE APPROACH OFFERS LOWER SYSTEM MASS AND REDUCES OVERALL SYSTEM TECHNICAL RISK. OUR PROPOSED PATENTED THIN PANEL DESIGN IS AN EFFICIENT SOLAR ARRAY STRUCTURE THAT WILL ACHIEVE A SPECIFIC POWER GREATER THAN 140 WATTS/KILOGRAM (W/KG). THE ARRAY PROVIDES OUTWARD FACING CELLS WHEN STOWED SO THAT POWER CAN BE GENERATED BEFORE ARRAY DEPLOYMENT. THE LOW PROFILE PANCAKE GIMBAL SUPPORTS GENERATING MAXIMUM AVERAGE POWER DURING THE MISSION. Other Administrative Action $0 5/31/18 8 THESE SYSTEM TECHNICAL DRIVERS ALIGN WELL WITH THE INHERENT CAPABILITIES OF OUR HIGH WATTS PER KILOGRAM (HAWK) SOLAR ARRAY THAT HAS COMPLETED QUALIFICATION AND IS AWAITING SPACECRAFT INTEGRATION ON THE AFRL BIARRI MISSION CURRENTLY SCHEDULED FOR LAUNCH IN Q4 2015. WE WILL LEVERAGE SIGNIFICANTLY FROM THE EXISTING HAWK DESIGN AND RISK REDUCTION EFFORTS ALREADY NEARING COMPLETION ON OUR AIR FORCE PROGRAM. OUR PROPOSED SOLAR ARRAY SYSTEM DESIGN MEETS ALL OF THE LISTED REQUIREMENTS. OUR INNOVATIVE APPROACH OFFERS LOWER SYSTEM MASS AND REDUCES OVERALL SYSTEM TECHNICAL RISK. OUR PROPOSED PATENTED THIN PANEL DESIGN IS AN EFFICIENT SOLAR ARRAY STRUCTURE THAT WILL ACHIEVE A SPECIFIC POWER GREATER THAN 140 WATTS/KILOGRAM (W/KG). THE ARRAY PROVIDES OUTWARD FACING CELLS WHEN STOWED SO THAT POWER CAN BE GENERATED BEFORE ARRAY DEPLOYMENT. THE LOW PROFILE PANCAKE GIMBAL SUPPORTS GENERATING MAXIMUM AVERAGE POWER DURING THE MISSION. Other Administrative Action $100.1k 3/21/18 7 THESE SYSTEM TECHNICAL DRIVERS ALIGN WELL WITH THE INHERENT CAPABILITIES OF OUR HIGH WATTS PER KILOGRAM (HAWK) SOLAR ARRAY THAT HAS COMPLETED QUALIFICATION AND IS AWAITING SPACECRAFT INTEGRATION ON THE AFRL BIARRI MISSION CURRENTLY SCHEDULED FOR LAUNCH IN Q4 2015. WE WILL LEVERAGE SIGNIFICANTLY FROM THE EXISTING HAWK DESIGN AND RISK REDUCTION EFFORTS ALREADY NEARING COMPLETION ON OUR AIR FORCE PROGRAM. OUR PROPOSED SOLAR ARRAY SYSTEM DESIGN MEETS ALL OF THE LISTED REQUIREMENTS. OUR INNOVATIVE APPROACH OFFERS LOWER SYSTEM MASS AND REDUCES OVERALL SYSTEM TECHNICAL RISK. OUR PROPOSED PATENTED THIN PANEL DESIGN IS AN EFFICIENT SOLAR ARRAY STRUCTURE THAT WILL ACHIEVE A SPECIFIC POWER GREATER THAN 140 WATTS/KILOGRAM (W/KG). THE ARRAY PROVIDES OUTWARD FACING CELLS WHEN STOWED SO THAT POWER CAN BE GENERATED BEFORE ARRAY DEPLOYMENT. THE LOW PROFILE PANCAKE GIMBAL SUPPORTS GENERATING MAXIMUM AVERAGE POWER DURING THE MISSION. Other Administrative Action $0 1/2/18