Unleash Your Potential
Introducing DROID.alphaTM
Traditional hosted payload solutions often present challenges due to misaligned incentives between platform providers and bus suppliers.
These complexities can introduce unnecessary friction and limitations, hindering your mission's full potential.
We Remove the Complex.
SIMPLICITY
Our Satellites Are NOT Configurable
Control your DROID via STARFIRE OSTM tasking APIs
SECURITY
End-to-End Data Encryption
RELIABILITY
We Handle
Day-to-Day Operations
FOCUS
One Client
Per Satellite
We Focus on What Matters.
DROID.alphaTM
Time to Launch:18 months
Orbits:LEO / GEO
Mission Life:10 / 5 yrs
Mechanical Configuration
Payload Volume:1000mm x 1100mm x 510mm
Bus Mass:135 kg
Max Payload Mass:165 kg
PropulsionHall Effect Thruster
Thrust:9mN
Delta-V (Bus):1673 m/s
Delta-V (Max Payload):706 m/s
Electrical Power System
Peak Power Generation:552 W
Array Configuration:Gimballed
Payload OAP (550km Orbit):280 W
Battery Capacity:1.15 kW-Hr
ADCS
Slew Rates:X: 5°/s Y: 5°/s Z: 5°/s
Pointing Accuracy:10 arcsecond 1-σ
Communications
Downlink (TT&C):0.510 Mbps
Uplink (TT&C):0.128 Mbps
Downlink (Mission Data):400 Mbps
Real-Time Communications:0.150 Mbps*
DROID.alphaTMENHANCED MOBILITY
Time to Launch:24 months
Orbits:vLEO / LEO / GEO / Cislunar
Mission Life:5 / 10 / 5 / 5 yrs
Mechanical Configuration
Payload Volume:1000mm x 1100mm x 1000mm
Bus Mass:250 kg
Max Payload Mass:250 kg
PropulsionTIE-20
Thrust:44mN
Delta-V (Bus):>10 km/s
Delta-V (Max Payload):>10 km/s
Electrical Power System
Peak Power Generation:1130 W
Array Configuration:Gimballed
Payload OAP (550km Orbit):680 W
Battery Capacity:3.42 kW-Hr
ADCS
Slew Rates:X: 4°/s Y: 4°/s Z: 4°/s
Pointing Accuracy:10 arcsecond 1-σ
Communications
Downlink (TT&C):0.510 Mbps
Uplink (TT&C):0.128 Mbps
Downlink (Mission Data):400 Mbps
Real-Time Communications:0.150 Mbps*