MTQ800 DATASHEET Product enquiry MTQ800 cad model

MTQ800 Magnetorquers

Precise performance at high efficiency. The MTQ800 magnetorquers are aimed at applications in 50-200 kg class satellites.

Offering one of the highest energy efficiencies in the industry, combined with fine-grained dipole-moment strength control, it allows precise pointing and rapid de-saturation of any reaction wheels in the satellite.

With a unique boost-mode, these magnetorquers can be pushed up to higher magnetic dipole moments for short duration manoeuvres, through sacrificing some energy efficiency. In return, these magnetorquers will offer the fastest de-tumbling of any satellite in this mass class, allowing the users to start their operations in the shortest amount of time. The MTQ800 Magnetorquers feature an inherently safe, passive detumbling mode, which works without any external controller.

Compatibility

The MTQ800 series is compatible with AAC Hyperion’s portfolio of Attitude Determination and Control products.

Adaptability

Dipole moment directly controllable, in steps of 1 mA.m². In addition the controller can be tuned for faster/slower operation.

Heritage

The MTQ800 magnetorquer series has been flying on numerous missions since 2020 and is at TRL 9. It is based on AAC Hyperion’s experience in design and development of magnetorquers for CubeSats which have been flying since 2017.

Why the MTQ800 Magnetorquers?

  • TRL 9
  • 16-20 Week Lead Time
  • Flown Since 2020
  • Includes drive electronics and mounting brackets
  • Nominal dipole moment: 15 A.m2
  • Boost mode dipole moment: up to 30 A.m²
  • Dimensions: 25 mm 250 mm (Ø x l)
  • Mass: 395 g
  • Dipole moment directly controllable, in steps of 1 mA.m²
  • RS422 Interface
  • Power consumption at nominal dipole moment only 3 W, including drive electronics
  • Inherently safe, passive detumbling mode

Technical Specifications

Environmental
Operating temperature range -45 - +45 °C
Maximum acceleration load 10 (TBC) X-axis; g
10 (TBC) Y-axis; a
10 (TBC) Z-axis; g
Electrical specifications
Design dipole moment 15 Am
Peak dipole moment 30 Am
Control accuracy (Design dipole moment) +/- 2 % (of setpoint)
Control accuracy (Peak dipole moment) +/-10 % (of setpoint)
Supply voltage
Min. Typ. Max.
Supply voltage (V) 8 12 12.5
Power and current consumption
Min. Typ. Max.
Idle (mW) 144 156 180
Dipole moment of 10 Am (mW) 1440 1536 1632
Dipole moment of 20 Am (mW) 4800 5040 5520
Maximum dipole moment (mW) 13200

Related products

ANT-GPS-A
AAC SpaceQuest

ANT-GPS Series

The ANT-GPS-Series Antenna is a space qualified L-band patch antenna tuned to the GPS frequency bands. This antenna is ideal for MicroSats and SmallSats but can also be mounted recessed on CubeSats.
GNSS-701
AAC SpaceQuest

GNSS-701

The AAC SpaceQuest GNSS-701 is a compact yet powerful satellite GNSS receiver, and is one of AAC SpaceQuest’s bestselling components of all time.
iADCS200
AAC Hyperion

iADCS200

Our plug-and-play iADCS200 range of fully integrated attitude control systems are flight proven with low power requirements.
IADCS400
AAC Hyperion

iADCS400

The iADCS400 is a fully autonomous attitude determination and control system aimed at small satellites with a 6U CubeSat form factor or larger
MAG-3
AAC SpaceQuest

MAG-3

The MAG-3 Three Axis Satellite Magnetometer enables reliable and accurate spacecraft attitude measurements.
MM200
AAC Hyperion

MM200

The MM200 is a high precision magnetometer suited for autonomous satellite attitude control or scientific measurements
NANOSSOC-D60
AAC SpaceQuest

nanoSSOC-D60

nanoSSOC-D60 is a AAC SpaceQuest Developed two-axis and low-cost sun sensor for high accurate sun-tracking, pointing and attitude determination.
PG400 GYROSCROPE
AAC Hyperion

PG400 GYROSCOPE

The PG400 gyroscope hosts an impressive Angular Random Walk of 0.23 deg/sqrt(Hz) and a bias instability of 1 deg/hr. This high-performance component utilises a RS422 interface with a request-based protocol for command and data handling, enabling seamless integration with your platform design.
RW210
AAC Hyperion

RW222

Our next generation high-performance RW222 reaction wheels are ideal for highly agile small satellite missions requiring precision pointing.
rw400 reaction wheel
AAC Hyperion

RW400

Our high-performance reaction wheels are ideal for agile small satellite missions requiring accurate pointing.
SS200
AAC Hyperion

SS200

Miniaturised digital sun sensor with high accuracy and 110 deg FOV
SSOC-D60
AAC SpaceQuest

SSOC-D60

The SSoC-D60 SmallSat Satellite Sun Sensor with digital interface is a low-cost sun sensor for high accurate sun-tracking, pointing and attitude determination.
ST200
AAC Hyperion

ST200

Our ST200 CubeSat star tracker offers attitude determination in an incredibly small package. The ST200, developed by AAC Hyperion, is one of the world’s smallest and lightest fully autonomous, low power star trackers, aimed at applications in pico- and nano-satellite platforms
ST400-T
AAC Hyperion

ST400

Powerful attitude determination for small satellites. The ST400 star tracker, developed by AAC Hyperion, is aimed at microsatellite systems. With increased attitude determination accuracy and improved radiation tolerance compared to its little brother, the ST200, it enables more demanding missions.
Trillian-1

Trillian-1

For maximum accuracy & reliability. The Trillian-1 reaction wheel provides high reliability, adaptability, and accuracy making it a one-of-a-kind product for Small Satellite missions.

Enquire about this product

"*" indicates required fields

Name*