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Table Of Contents

Integrate ADCS

with Spherical Motor Technology

Installation Interfaces

Specifications

Environmental Tests

following ESA QB50

1. Weight: < 400g

2. Dynamic Balance: < G0.4

3. Max. Power Consumption: 1W

4. Pointing Accuracy: 0.2 deg when

the sun is capturable; 1 deg when

the sun is not capturable

5. Max. Momentum: 10 mNms

6. Max. Torque: 1mNm

7. Interface: I2C, UART

8. Lead Time: 4 weeks

Description

With patented magnetic field design and control methodology,

this device is capable of providing angular momentum and

magnetic dipole in 3 axis. This brings your satellite ADCS same

performance but one-third of the weight, volume, and power

consumption compared to the traditional system.

1 Spherical Motor serves

as 3 single-axis reaction

wheels and 3 torquers

Sun sensor, and Tactical

Grade Gyro included

Configuration 1. Install in the bottom of

3U+ / 6U+ Satellite (Hockey Part)

# Occupied Volume: 0.2U

Configuration 2. Install in

the middle of CubeSat

# Occupied Volume: 0.4U

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Integrate ADCS with Spherical Motor Technology Environmental Tests f ollowing ESA QB50 1 Spherical Motor ser ves as 3 single-axis reaction wheels and 3 torquers Sun sensor , and T actical Grade Gyro included Description Specifications With patented magnetic field design and control methodology, this device is capable of providing angular momentum and magnetic dipole in 3 axis.
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Spherical Motor Technology Unlike traditional single-axis reaction wheel motor, 1 spherical motor is capable of providing angular momentum in 3 axes. In addition, by applying bias currents, it acts as 3 single-axis magnetorquers as well. In terms of rotational dynamics, it is actually a control moment gyro.