Key highlights

MN200 is a platform with high-performance on remote sensing which is developed by MINOSpace. Based on the mature design of OBDH and attitude control system, it focuses on improving the carrying capacity of the payload and pointing accuracy. The propulsion system can be optional for the stability of attitude and orbit maintenance of the satellite, meeting the requirements of the design life for about 3~5 years.

With the synthetic aperture radar (SAR) or optical very-high-resolution imager (VHRI) payload, the MN200 satellite can obtain 0.5m@500km ultra-high-resolution ground remote sensing images.

Main feature

◼ Standardized design for platform and adaptive to the requirements of various optical /SAR payloads.

◼ Lightweight design for platform, high payload fraction.

◼ Integrated design for electronic equipment, reducing internal interface, reduce the launch mass of satellite.

◼ Short production cycle, and the delivery is about 18 months

Disclaimer: satsearch is not responsible for any mistakes on this page, although we do our best to ensure correctness. Please report any mistakes to us.

Last updated: 2020-09-14

MN200 platform

Downloads

Export

  • Click here to add the MinoSpace - MN200 platform to the Valispace engineering tool from satsearch
  • Click here to add the MinoSpace - MN200 platform to Lynapse Studio by Spacebackend
  • Click here to add the MinoSpace - MN200 platform to 360 by IENAI

from our blog

Go to blog

Microsatellite and CubeSat platforms on the global market

Find a launch option for your CubeSat or small satellite - an overview of launch service providers

Optical payloads for small satellites: a sector overview