3U/4U

6U

12U

 

3U/4U Spacecraft

Capabilities and Specifications:

• Compatible with all common dispensers
• 40W solar array power
• Mission-specific fixed, deployable, or articulated solar panels
• 1.5U payload volume
• 8A @ 3.3V, 5V, 12V, 3-55V; 10A @ VBATT (16.8V); 400W Max power distribution
  
• 100-200 Whr @ 16.8V energy storage
  
• Up to 32 GB flash memory
• 20 arcsec pointing knowledge
• .01° @ 0.001°/s pointing accuracy
  
• Consistent interface for bus telemetry and telecommands across all modules; Engineering units (mV, mA, 0.1K)
  
• 1GHz ARM Processor; Linux Based OS
  
• Flight certified under NASA GEVS
  
• 555 channels L1 GPS Standard, all other constellations and frequencies optional
  
• 4m position, 0.05 m/s velocity knowledge with on-board orbit propagator
  
• Data Bus: I2C, GPIO, UART, SPI, RS-422, RS-232, USB, Ethernet 
  
• Communications: CCSDS, TCP-IP, UDP; UHF, L-/S-/X-band options available
  
• 9B/s (beacon), 9.6 kbps, 4/20/100 Mbps data rates
  
• AES256 and other encryption available
  
• Python, C, and C++ development languages
• Compatible with propulsion systems
• Up to 5 years LEO lifetime
• Bus specification tailored to customer requirements
  

 

6U Spacecraft

Capabilities and Specifications:

• Compatible with CSD and NanoRacks dispensers
• 64W solar array power
• Mission-specific fixed, deployable, or articulated solar panels
• 4U payload volume
• 8A @ 3.3V, 5V, 12V, 3-55V; 10A @ VBATT (16.8V); 400W Max power distribution
• 100-200 Whr @ 16.8V energy storage
• Up to 32 GB flash memory
• 20 arcsec pointing knowledge
• .01° @ 0.001°/s pointing accuracy
• Consistent interface for bus telemetry and telecommands across all modules; Engineering units (mV, mA, 0.1K)
• 1GHz ARM Processor; Linux Based OS
• Flight certified under NASA GEVS
• 555 channels L1 GPS Standard, all other constellations and frequencies optional
• 4m position, 0.05 m/s velocity knowledge with on-board orbit propagator
• Data Bus: I2C, GPIO, UART, SPI, RS-422, RS-232, USB, Ethernet 
• Communications: CCSDS, TCP-IP, UDP; UHF, L-/S-/X-band options available
• 9B/s (beacon), 9.6 kbps, 4/20/100 Mbps data rates
• AES256 and other encryption available
• Python, C, and C++ development languages
• Compatible with propulsion systems
• Up to 5 years LEO lifetime
• Bus specification tailored to customer requirements

 

12U Spacecraft

Capabilities and Specifications:

• Compatible with CSD, NanoRacks, and Lightband dispensers
• 110W solar array power
• Mission-specific fixed, deployable, or articulated solar panels
• 9.5U payload volume
• 8A @ 3.3V, 5V, 12V, 3-55V; 10A @ VBATT (16.8V); 400W Max power distribution
• 100-200 Whr @ 16.8V energy storage
• Up to 32 GB flash memory
• 20 arcsec pointing knowledge
• 1° @ 0.01°/s pointing accuracy
• Consistent interface for bus telemetry and telecommands across all modules; Engineering units (mV, mA, 0.1K)
• 1GHz ARM Processor; Linux Based OS
• Flight certified under NASA GEVS
• 555 channels L1 GPS Standard, all other constellations and frequencies optional
• 4m position, 0.05 m/s velocity knowledge with on-board orbit propagator
• Data Bus: I2C, GPIO, UART, SPI, RS-422, RS-232, USB, Ethernet 
• Communications: CCSDS, TCP-IP, UDP; UHF, L-/S-/X-band options available
• 9B/s (beacon), 9.6 kbps, 4/20/100 Mbps data rates
• AES256 and other encryption available
• Python, C, and C++ development languages
• Compatible with propulsion systems
• Up to 5 years LEO lifetime
• Bus specification tailored to customer requirements