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We are focused on affordability, performance and flexibility to deliver autonomous, dynamic spacecraft for our customers’ missions. We offer highly agile and maneuverable small satellites that are flexible to host different payloads across orbits. And the onboard processing we’ve developed has proven to be orders of magnitude better than heritage systems.
ISR
ADV. SPACE*
COMMS*
MW/MD
COMMS*
MW/MD
ADV. SPACE*
COMMS*
We can design to any requirements in low Earth orbit. We can provide one-to-three-year lifetimes or three-to-seven-year lifetimes with selective-redundancy approaches. Our systems offer green, monopropellant and bipropellant propulsion.
10kg - 1,000kg Class
Up to 500 w
12u to ESPA Grande typical
We can design to any requirements in medium Earth orbit. We can provide one-to-three-year lifetimes or three-to-seven-year lifetimes with selective-redundancy approaches. Our systems are rated to MEO radiation environments and offer electric, monopropellant and bipropellant propulsion.
50kg - 3,000kg Class
Up to 4,000 w
1/2 ESPA to launch-vehicle limited
We can design to any requirements in geosynchronous orbit. We can provide small satellites with three-to-five-year lifetimes with single-string avionics or five-to-seven-year lifetimes with selective-redundancy approaches. Our systems are rated to GEO radiation environments and offer electric, monopropellant and bipropellant propulsion..
50kg - 3,000kg Class
Up to 4,000 w
1/2 ESPA to launch-vehicle limited
With lower cost launch and manned-missions to the moon, the econosphere in cis-lunar space will grow. The need to service and protect this new space operations domain will grow over time. The orbit agnostic capabilities we’ve developed are easily transitioned to cis-lunar.
Future small satellite opportunities are in V-LEO, or very-low Earth orbit, approximately 150 km above Earth. V-LEO utility includes quick missions for tactical support. These systems operate much closer to the ground and have very short mission lives, resulting in lower all-around costs. Tactically relevant capabilities tailored for theater operations for specific time periods is a new market opportunity.
We can design to any requirements in geosynchronous orbit. We can provide small satellites with three-to-five-year lifetimes with single-string avionics or five-to-seven-year lifetimes with selective-redundancy approaches. Our systems are rated to GEO radiation environments and offer electric, monopropellant and bipropellant propulsion.
50kg - 3,000kg Class
Up to 4,000 w
1/2 ESPA to launch-vehicle limited
WFOV Space Program, Set for 2022 Launch
We can design to any requirements in medium Earth orbit. We can provide one-to-three-year lifetimes or three-to-seven-year lifetimes with selective-redundancy approaches. Our systems are rated to MEO radiation environments and offer electric, monopropellant and bipropellant propulsion.
50kg - 3,000kg Class
Up to 4,000 w
1/2 ESPA to launch-vehicle limited
WFOV Space Program, Set for 2022 Launch
We can design to any requirements in low Earth orbit. We can provide one-to-three-year lifetimes or three-to-seven-year lifetimes with selective-redundancy approaches. Our systems offer green, monopropellant and bipropellant propulsion.
10kg - 1,000kg Class
Up to 500 w
12u to ESPA Grande typical
WFOV Space Program, Set for 2022 Launch
Future small satellite opportunities are in V-LEO, or very-low Earth orbit, approximately 150 km above Earth. V-LEO utility includes quick missions for tactical support. These systems operate much closer to the ground and have very short mission lives, resulting in lower all-around costs. Tactically relevant capabilities tailored for theater operations for specific time periods is a new market opportunity.
With lower cost launch and manned-missions to the moon, the econosphere in cis-lunar space will grow. The need to service and protect this new space operations domain will grow over time. The orbit agnostic capabilities we’ve developed are easily transitioned to cis-lunar.
We develop single small satellites to support development programs and to prototype phenomenologies and/or mission payloads.
We develop collaborative small satellites and operations, with a minimum of three small satellites.
We develop large constellations based on our single satellites and small constellation designs.
