Microsatellite Bus MP42 - NanoAvionics

Check-in is open for Newspace 3.0

Be part of the future with us!

Register now for our online product launch event on May 23rd.

Microsatellite Bus MP42

Microsatellite Bus MP42

Get Access to NanoAvionics Product Catalog with Tech Specs

Microsatellites can offer extremely high levels of performance and reliability across various space applications. From high-resolution Earth Observation (EO) cameras to powerful space-based internet services, microsatellites have the potential to generate significant value for modern industries.

NanoAvionics’ proven, mid-range microsatellite bus, the MP42, uses a 15″ ESPA-class separation ring and can accommodate payloads with a maximum mass of 60 kg and a total footprint of 572(L) x 460(W) x 370(H)* mm. *Payload height is flexible, as long as the total satellite height does not exceed the launch vehicle’s allowable volume. The large payload envelope provides flexibility for deployable antennas, booms, and other structures.

NanoAvionics offers three standard MP42 microsatellite performance configurations – Light, Mid, and Max – providing options that best match customers’ payload, mission objectives, and budget.

The system’s mission operations infrastructure, hardware and software elements have all been built to act as mission-specific building blocks, based on a baseline architecture that has been optimized for high-performance missions. This saves time and resources during integration by providing simpler and more repeatable processes.

The platform is also provided loaded with sample mission code (which is easily customized, extended, or replaced) and pre-qualified for fast flight acceptance testing, subject to mission requirements.

The MP42 platform is a versatile system and has been optimized for high data throughput and complex communications missions and services. It is also suitable for research projects, emergency communications, and remote sensing services, and can be adapted to such applications with minimal reconfiguration.

Drag to sides
Request information

Get Access to NanoAvionics Product Catalog with Tech Specs

Microsatellites can offer extremely high levels of performance and reliability across various space applications. From high-resolution Earth Observation (EO) cameras to powerful space-based internet services, microsatellites have the potential to generate significant value for modern industries.

NanoAvionics’ proven, mid-range microsatellite bus, the MP42, uses a 15″ ESPA-class separation ring and can accommodate payloads with a maximum mass of 60 kg and a total footprint of 572(L) x 460(W) x 370(H)* mm. *Payload height is flexible, as long as the total satellite height does not exceed the launch vehicle’s allowable volume. The large payload envelope provides flexibility for deployable antennas, booms, and other structures.

NanoAvionics offers three standard MP42 microsatellite performance configurations – Light, Mid, and Max – providing options that best match customers’ payload, mission objectives, and budget.

The system’s mission operations infrastructure, hardware and software elements have all been built to act as mission-specific building blocks, based on a baseline architecture that has been optimized for high-performance missions. This saves time and resources during integration by providing simpler and more repeatable processes.

The platform is also provided loaded with sample mission code (which is easily customized, extended, or replaced) and pre-qualified for fast flight acceptance testing, subject to mission requirements.

The MP42 platform is a versatile system and has been optimized for high data throughput and complex communications missions and services. It is also suitable for research projects, emergency communications, and remote sensing services, and can be adapted to such applications with minimal reconfiguration.

  • MP42 15" Light Specifications
    • Bus power (Sun tracking): 218 W
    • Available Payload mass (payload adaptor plate mass is included in the payload mass budget): 60 kg
    • Available Payload volume: 572(L) x 460(W) x 370(H)* mm

    *Payload height is dependent on the launch vehicle’s allowable volume and shall be confirmed with KNA in advance.

    • Max Allowable S/C mass: 150 kg
    • Data rates and Frequencies:
      • UHF:
        • 401-402 MHz
        • Uplink/Downlink 1.6 kpbs
      • 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)
    • Deployment ring: 15″
    • Battery capacity: 852 Wh
    • Payload voltage channels:
      • Regulated voltage rails: 3.3, 5.0, 12.0, 28.0 V
      • Unregulated rails:
      • (Vbat, 4S): 12-16 V
      • (Vbat, 8S): 24 – 33.2 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: 7 mN Hall Effect Thruster
  • MP42 15" Mid Specifications
    • Bus power (Sun tracking): 218 W
    • Available Payload mass (payload adaptor plate mass is included in the payload mass budget): 60 kg
    • Available Payload volume: 572(L) x 460(W) x 370(H)* mm

    *Payload height is dependent on the launch vehicle’s allowable volume and shall be confirmed with KNA in advance.

    • Max Allowable S/C mass: 150 kg
    • Data rates and Frequencies:
      • UHF:
        • 401-402 MHz
        • Uplink/Downlink 1.6 kpbs
      • S-band:
        • Uplink 2025-2110 MHz; 53 kbps
        • Downlink 2200-2290 MHz; 3 Mbps
      • X-band:
        • Downlink 8025-8400 MHz
        • From PC Memory 80 Mbps
        • Routing from Payload up to 200 Mbps
    • Absolute knowledge error: 4.31° (1σ)
    • Absolute performance error: 4.40° (1σ)
    • Deployment ring: 15″
    • Battery capacity: 852 Wh
    • Payload voltage channels:
      • Regulated voltage rails: 3.3, 5.0, 12.0, 28.0 V
      • Unregulated rails:
      • (Vbat, 4S): 12-16 V
      • (Vbat, 8S): 24 – 33.2 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: 7 mN Hall Effect Thruster
  • MP42 15" Max Specifications
    • Bus power (Sun tracking): 218 W
    • Available Payload mass (payload adaptor plate mass is included in the payload mass budget): 60 kg
    • Available Payload volume: 572(L) x 460(W) x 370(H)* mm

    *Payload height is dependent on the launch vehicle’s allowable volume and shall be confirmed with KNA in advance.

    • Max Allowable S/C mass: 150 kg
    • Data rates and Frequencies:
      • UHF:
        • 401-402 MHz
        • Uplink/Downlink 1.6 kpbs
      • S-band:
        • Uplink 2025-2110 MHz; 53 kbps
        • Downlink 2200-2290 MHz; 3 Mbps
      • X-band:
        • Downlink 8025-8400 MHz
        • From PC Memory 80 Mbps
        • Routing from Payload up to 200 Mbps
    • Absolute knowledge error**: 0.03° (1σ)
    • Absolute performance error**: 0.08° (1σ)

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

    • Deployment ring: 15″
    • Battery capacity: 852 Wh
    • Payload voltage channels:
      • Regulated voltage rails: 3.3, 5.0, 12.0, 28.0 V
      • Unregulated rails:
      • (Vbat, 4S): 12-16 V
      • (Vbat, 8S): 24 – 33.2 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: 7 mN Hall Effect Thruster
Highlighted Missions
NanoAvionics

Client name

Multiple clients - rideshare

Launch date

2022.04.01

MP42 is NanoAvionics’ largest satellite built and launched so far, based on one of the first commercially available modular microsatellite buses in the industry. MP42 is a rideshare mission, and part of the company’s ongoing program. It’s hosting multiple payloads including OQ Technology’s “Tiger-3”, adding another satellite to its 5G IoT/M2M (machine-to-machine) communication constellation, and VeoWare’s RW500 fully integrated reaction wheel.

Read more about MP42 mission

  • MP42 15" Light Specifications
    • Bus power (Sun tracking): 218 W
    • Available Payload mass (payload adaptor plate mass is included in the payload mass budget): 60 kg
    • Available Payload volume: 572(L) x 460(W) x 370(H)* mm

    *Payload height is dependent on the launch vehicle’s allowable volume and shall be confirmed with KNA in advance.

    • Max Allowable S/C mass: 150 kg
    • Data rates and Frequencies:
      • UHF:
        • 401-402 MHz
        • Uplink/Downlink 1.6 kpbs
      • 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)
    • Deployment ring: 15″
    • Battery capacity: 852 Wh
    • Payload voltage channels:
      • Regulated voltage rails: 3.3, 5.0, 12.0, 28.0 V
      • Unregulated rails:
      • (Vbat, 4S): 12-16 V
      • (Vbat, 8S): 24 – 33.2 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: 7 mN Hall Effect Thruster
  • MP42 15" Mid Specifications
    • Bus power (Sun tracking): 218 W
    • Available Payload mass (payload adaptor plate mass is included in the payload mass budget): 60 kg
    • Available Payload volume: 572(L) x 460(W) x 370(H)* mm

    *Payload height is dependent on the launch vehicle’s allowable volume and shall be confirmed with KNA in advance.

    • Max Allowable S/C mass: 150 kg
    • Data rates and Frequencies:
      • UHF:
        • 401-402 MHz
        • Uplink/Downlink 1.6 kpbs
      • S-band:
        • Uplink 2025-2110 MHz; 53 kbps
        • Downlink 2200-2290 MHz; 3 Mbps
      • X-band:
        • Downlink 8025-8400 MHz
        • From PC Memory 80 Mbps
        • Routing from Payload up to 200 Mbps
    • Absolute knowledge error: 4.31° (1σ)
    • Absolute performance error: 4.40° (1σ)
    • Deployment ring: 15″
    • Battery capacity: 852 Wh
    • Payload voltage channels:
      • Regulated voltage rails: 3.3, 5.0, 12.0, 28.0 V
      • Unregulated rails:
      • (Vbat, 4S): 12-16 V
      • (Vbat, 8S): 24 – 33.2 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: 7 mN Hall Effect Thruster
  • MP42 15" Max Specifications
    • Bus power (Sun tracking): 218 W
    • Available Payload mass (payload adaptor plate mass is included in the payload mass budget): 60 kg
    • Available Payload volume: 572(L) x 460(W) x 370(H)* mm

    *Payload height is dependent on the launch vehicle’s allowable volume and shall be confirmed with KNA in advance.

    • Max Allowable S/C mass: 150 kg
    • Data rates and Frequencies:
      • UHF:
        • 401-402 MHz
        • Uplink/Downlink 1.6 kpbs
      • S-band:
        • Uplink 2025-2110 MHz; 53 kbps
        • Downlink 2200-2290 MHz; 3 Mbps
      • X-band:
        • Downlink 8025-8400 MHz
        • From PC Memory 80 Mbps
        • Routing from Payload up to 200 Mbps
    • Absolute knowledge error**: 0.03° (1σ)
    • Absolute performance error**: 0.08° (1σ)

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

    • Deployment ring: 15″
    • Battery capacity: 852 Wh
    • Payload voltage channels:
      • Regulated voltage rails: 3.3, 5.0, 12.0, 28.0 V
      • Unregulated rails:
      • (Vbat, 4S): 12-16 V
      • (Vbat, 8S): 24 – 33.2 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: 7 mN Hall Effect Thruster