CubeADCS Y-Momentum

ADCS System by CubeSpace (1 more product)

Note : Your request will be directed to CubeSpace.

CubeADCS Y-Momentum Image

The CubeADCS from CubeSpace is a low-power Attitude Determination and Control System (ADCS) that is designed for use in nanosatellites with a form factor of 2 to 16 U and can be configured for use in large satellites. It has a mass of less than 0.3 Kg. It consists of an ADCS computer with a 3-axis MEMS rate sensor, a deployable magnetometer, coarse sun sensors, a redundant magnetometer, fine sun & earth sensors, and a star tracker. This ADCS system has three default modes that can provide detumbling of the satellite, attitude stabilization in the orbit, and perform pitch maneuvers. This system measures 90 x 96 x 48 mm.

Product Specifications

Product Details

  • Part Number
    CubeADCS Y-Momentum
  • Manufacturer
    CubeSpace
  • Description
    ADCS for Nadir Pointing and Orientation Control for CubeSats

General Parameters

  • Satellite Type
    CubeSat
  • Component
    Torquer Coil, Torquer Rod, Sun Sensor, Magnetometer, Reaction Wheel, Star Tracker
  • Mass
    0.3 kg
  • Supply Voltage
    3.3V, 5V, VBat (6.5V -16V)
  • Power Consumption
    571 to 2295 mW
  • Radiation Tolerance
    20 Krad
  • Data Interface
    I2C, UART, CAN
  • Operating Temperature
    -10 to 60 Degree C
  • Dimension
    90 x 96 x 48 mm
  • Application
    Nadir Pointing, orientation control, detumbling of the satellite, attitude stabilization in the orbit, and perform pitch maneuvers

Technical Documents