8U Nanosatellite Bus M8P - NanoAvionics

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8U Nanosatellite Bus M8P

8U Nanosatellite Bus M8P

Get Access to NanoAvionics Product Catalog with Tech Specs

NanoAvionics offers three standard M8P nanosatellite performance configurations – Light, Mid, and Max – providing options that best match customers’ payload, mission objectives, and budget. The standardized setups enable engineers to spend more development time and resources on high-level tasks, such as payload development and its support during operations.

Modern 8U CubeSats can provide significant levels of performance and data resolution with the advanced subsystems on today’s market. Our M8P is a powerful, pre-configured platform to support such technologies and has been specifically designed for optimum performance in demanding commercial settings.

For engineers assessing 6U options, note that this 8U is a viable alternative. The M8P can provide very similar average orbit power to a 16U nanosatellite, and improve mission capabilities and redundancy at only marginally increased production and launch costs compared to the M6P.

The bus has a modular design, making it simple to adapt and extend, depending on the mission requirements, and the system can be used for a diverse array of applications, as a solo satellite or in a constellation, including:

  • Commercial and emergency communication services,
  • Internet of Things (IoT) and Machine-to-Machine (M2M) applications,
  • Earth Observation (EO) services, scientific and research missions,
  • Automatic Dependent Surveillance–Broadcast (ADS-B) aviation traffic monitoring and control, and
  • Automatic Identification Systems (AIS) maritime traffic monitoring and control.

Beyond such primary mission objectives, a propulsion system enables greater versatility and extended operational lifetimes. This includes high-impulse maneuvers for collision avoidance, re-positioning, orbital changes, de-orbiting, precision flight formations, and atmospheric drag compensation.

All onboard systems also utilize radiation-tolerant components and have been carefully designed to enable both precise thermal control and robust, consistent power delivery.

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Get Access to NanoAvionics Product Catalog with Tech Specs

NanoAvionics offers three standard M8P nanosatellite performance configurations – Light, Mid, and Max – providing options that best match customers’ payload, mission objectives, and budget. The standardized setups enable engineers to spend more development time and resources on high-level tasks, such as payload development and its support during operations.

Modern 8U CubeSats can provide significant levels of performance and data resolution with the advanced subsystems on today’s market. Our M8P is a powerful, pre-configured platform to support such technologies and has been specifically designed for optimum performance in demanding commercial settings.

For engineers assessing 6U options, note that this 8U is a viable alternative. The M8P can provide very similar average orbit power to a 16U nanosatellite, and improve mission capabilities and redundancy at only marginally increased production and launch costs compared to the M6P.

The bus has a modular design, making it simple to adapt and extend, depending on the mission requirements, and the system can be used for a diverse array of applications, as a solo satellite or in a constellation, including:

  • Commercial and emergency communication services,
  • Internet of Things (IoT) and Machine-to-Machine (M2M) applications,
  • Earth Observation (EO) services, scientific and research missions,
  • Automatic Dependent Surveillance–Broadcast (ADS-B) aviation traffic monitoring and control, and
  • Automatic Identification Systems (AIS) maritime traffic monitoring and control.

Beyond such primary mission objectives, a propulsion system enables greater versatility and extended operational lifetimes. This includes high-impulse maneuvers for collision avoidance, re-positioning, orbital changes, de-orbiting, precision flight formations, and atmospheric drag compensation.

All onboard systems also utilize radiation-tolerant components and have been carefully designed to enable both precise thermal control and robust, consistent power delivery.

  • M8P Light Specifications
    • Bus power (Sun tracking): 42 W
    • Available Payload mass: 7 kg
    • Available Payload volume: 4 U
    • Max Allowable S/C mass: 15 kg
    • Data rates and Frequencies:
      • UHF:
        • 401-402 MHz
        • Uplink/Downlink up to 2.4 kbps
      • S-band:
        • Uplink 2025-2110 MHz; 53 kbps
        • Downlink 2200-2290 MHz; 3 Mbps
    • Absolute knowledge error: 4.31° (1σ)
    • Absolute performance error: 4.40° (1σ)
    • Battery capacity: 161 Wh
    • Payload voltage channels: 3.3, 5.0, 12.0 V, 18.0-25.0 V, Vbat (6.0 – 8.4 V)
    • Data interfaces:
      • 1 x 100BASE-TX Ethernet
      • 1x CAN
      • 1 x RS-422 (on request RS-485)
      • 3 x SPI
      • 2 x USART/UART
      • 2 x I2C
    • Data storage: 4 GB NAND
    • Encryption: AES-256-GCM/CBC (On-board)
    • Propulsion: 0.12 mN Field Emission Electric Propulsion
  • M8P Mid Specifications
    • Bus power (Sun tracking): 42W
    • Available Payload mass: 6.5 kg
    • Available Payload volume: 3.5 U
    • Max Allowable S/C mass: 15 kg
    • Data rates and Frequencies:
      • UHF:
        • 401-402 MHz
        • Uplink/Downlink up to 2.4 kbps
      • S-band:
        • Uplink 2025-2110 MHz; 53 kbps
        • Downlink 2200-2290 MHz; 3 Mbps
      • X-Band
        • Downlink 8025-8400 MHz
        • Up to 98 Mbps
    • Absolute knowledge error: 4.31° (1σ)
    • Absolute performance error: 4.40° (1σ)
    • Battery capacity: 161 Wh
    • Payload voltage channels: 3.3, 5.0, 12.0 V, 18.0-25.0 V, Vbat (6.0 – 8.4 V)
    • Data interfaces:
      • 3 x IEEE 802.3 1000BASE-T
      • 1 x CAN
      • 3 x RS422/UART
      • 2 x SPI
      • 2 x I2C
      • Up to 20 x LVDS, GTP, GPIO
    • Data storage: 32 GB NAND
    • Encryption: AES-256-GCM/CBC (On-board)
    • Propulsion: 0.12 mN Field Emission Electric Propulsion
  • M8P Max Specifications
    • Bus power (Sun tracking): 42 W
    • Available Payload mass: 6.5 kg
    • Available Payload volume: 3.5 U
    • Max Allowable S/C mass: 15 kg
    • Data rates and Frequencies:
      • UHF:
        • 401-402 MHz
        • Uplink/Downlink up to 2.4 kbps
      • S-band:
        • Uplink 2025-2110 MHz; 53 kbps
        • Downlink 2200-2290 MHz; 3 Mbps
      • X-Band
        • Downlink 8025-8400 MHz
        • Up to 98 Mbps
    • Absolute knowledge error*: 0.04° (1σ)
    • Absolute performance error*: 0.06° (1σ)

    *APE and AKE values for fine determination are provided assuming Payload-AOCS sensor calibration is performed in-orbit.

    • Battery capacity: 161 Wh
    • Payload voltage channels: 3.3, 5.0, 12.0 V, 18.0-25.0 V, Vbat (6.0 – 8.4 V)
    • Data interfaces:
      • 3 x IEEE 802.3 1000BASE-T
      • 1 x CAN
      • 3 x RS422/UART
      • 2 x SPI
      • 2 x I2C
      • Up to 20 x LVDS, GTP, GPIO
    • Data storage: 32 GB NAND
    • Encryption: AES-256-GCM/CBC (On-board)
    • Propulsion: 0.12 mN Field Emission Electric Propulsion
  • M8P Light Specifications
    • Bus power (Sun tracking): 42 W
    • Available Payload mass: 7 kg
    • Available Payload volume: 4 U
    • Max Allowable S/C mass: 15 kg
    • Data rates and Frequencies:
      • UHF:
        • 401-402 MHz
        • Uplink/Downlink up to 2.4 kbps
      • S-band:
        • Uplink 2025-2110 MHz; 53 kbps
        • Downlink 2200-2290 MHz; 3 Mbps
    • Absolute knowledge error: 4.31° (1σ)
    • Absolute performance error: 4.40° (1σ)
    • Battery capacity: 161 Wh
    • Payload voltage channels: 3.3, 5.0, 12.0 V, 18.0-25.0 V, Vbat (6.0 – 8.4 V)
    • Data interfaces:
      • 1 x 100BASE-TX Ethernet
      • 1x CAN
      • 1 x RS-422 (on request RS-485)
      • 3 x SPI
      • 2 x USART/UART
      • 2 x I2C
    • Data storage: 4 GB NAND
    • Encryption: AES-256-GCM/CBC (On-board)
    • Propulsion: 0.12 mN Field Emission Electric Propulsion
  • M8P Mid Specifications
    • Bus power (Sun tracking): 42W
    • Available Payload mass: 6.5 kg
    • Available Payload volume: 3.5 U
    • Max Allowable S/C mass: 15 kg
    • Data rates and Frequencies:
      • UHF:
        • 401-402 MHz
        • Uplink/Downlink up to 2.4 kbps
      • S-band:
        • Uplink 2025-2110 MHz; 53 kbps
        • Downlink 2200-2290 MHz; 3 Mbps
      • X-Band
        • Downlink 8025-8400 MHz
        • Up to 98 Mbps
    • Absolute knowledge error: 4.31° (1σ)
    • Absolute performance error: 4.40° (1σ)
    • Battery capacity: 161 Wh
    • Payload voltage channels: 3.3, 5.0, 12.0 V, 18.0-25.0 V, Vbat (6.0 – 8.4 V)
    • Data interfaces:
      • 3 x IEEE 802.3 1000BASE-T
      • 1 x CAN
      • 3 x RS422/UART
      • 2 x SPI
      • 2 x I2C
      • Up to 20 x LVDS, GTP, GPIO
    • Data storage: 32 GB NAND
    • Encryption: AES-256-GCM/CBC (On-board)
    • Propulsion: 0.12 mN Field Emission Electric Propulsion
  • M8P Max Specifications
    • Bus power (Sun tracking): 42 W
    • Available Payload mass: 6.5 kg
    • Available Payload volume: 3.5 U
    • Max Allowable S/C mass: 15 kg
    • Data rates and Frequencies:
      • UHF:
        • 401-402 MHz
        • Uplink/Downlink up to 2.4 kbps
      • S-band:
        • Uplink 2025-2110 MHz; 53 kbps
        • Downlink 2200-2290 MHz; 3 Mbps
      • X-Band
        • Downlink 8025-8400 MHz
        • Up to 98 Mbps
    • Absolute knowledge error*: 0.04° (1σ)
    • Absolute performance error*: 0.06° (1σ)

    *APE and AKE values for fine determination are provided assuming Payload-AOCS sensor calibration is performed in-orbit.

    • Battery capacity: 161 Wh
    • Payload voltage channels: 3.3, 5.0, 12.0 V, 18.0-25.0 V, Vbat (6.0 – 8.4 V)
    • Data interfaces:
      • 3 x IEEE 802.3 1000BASE-T
      • 1 x CAN
      • 3 x RS422/UART
      • 2 x SPI
      • 2 x I2C
      • Up to 20 x LVDS, GTP, GPIO
    • Data storage: 32 GB NAND
    • Encryption: AES-256-GCM/CBC (On-board)
    • Propulsion: 0.12 mN Field Emission Electric Propulsion