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Spacecraft

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

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  • Home
  • Media
    • News
    • Blog
  • Products / Store
  • Salvo RTOS
  • Supporting Documents
  • Contact
  • About Us
  • Careers