Image of Space Inventor - Maximum Power Point Tracker // MPPT-P4 on the satsearch marketplace

Key highlights

The Space Inventor AOCS (Attitude and Orbit Control System) Computer (OBC-P4 + AOCS SW)  is a high-performance, scalable platform designed to ensure precise satellite orientation across all mission classes — from agile CubeSats to sub-arcsecond micro-satellites. It integrates advanced sensor fusion, robust control algorithms, and fault-tolerant hardware architecture to deliver exceptional reliability and precision in orbit.

Key features

  • Converter efficiency up to 95%

  • Buck converter topology

  • Up to 110W PV input power per MPPT

  • PV string input voltage from VBAT up to maximum 60V

  • 4x PV input channels with 1.2 A output current per channel

  • Data interface: Redundant CAN bus with CSP

  • Ruggedized enclosure for best thermal performance

  • Shielding for radiation and EMI reduction

  • Module measurements: (L, W, H): 93 x 93 x 8.75 mm

  • Suitable for microsatellites and CubeSats

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Last updated: 2026-01-08

Maximum Power Point Tracker // MPPT-P4

list price: 35,000 EUR

9TRL
Image of Space Inventor - Maximum Power Point Tracker // MPPT-P4 on the satsearch marketplace

Downloads

Technical specs

output current
1.2 A
battery pack voltage
< 60 V
mass
150 g
width
93 mm
length
93 mm
height
8.75 mm
data interface
CAN bus with CSP protocol

Export

  • Click here to add the Space Inventor - Maximum Power Point Tracker // MPPT-P4 to the Valispace engineering tool from satsearch
  • Click here to add the Space Inventor - Maximum Power Point Tracker // MPPT-P4 to Lynapse Studio by Spacebackend
  • Click here to add the Space Inventor - Maximum Power Point Tracker // MPPT-P4 to 360 by IENAI

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