Trillian-1

Trillian-1 Datasheet Product enquiry Trillian-1 cad model

Reaction Wheels

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.

The Trillian-1 has proven performance and reliability. The product is tested to NASA GEVS acceptance levels and features input filters that aid to reduce signal noise while a dedicated motor driver control circuit commands the Reaction Wheel safely. Designed for constellation deployment, each wheel produces a nominal 1.2 Nms momentum storage and 47 mNm maximum torque in a 1.5kg package and features three operations modes; Torque, Speed, and Direct DAC control.

Heritage

Trillian-1 has flown since 2019 with over 10 units sold. The design is based on around AAC Clyde Space’s extensive reaction wheel development experience proven across 10s of satellites. Each unit features integrated sensor and communications noise filters to increase accuracy and proprietary protection circuitry based on years of subsystem design experience ensuring the Trillian-1 will provide unparalleled mission assurance.

Adaptability

The Trillian-1 is constellation-ready and optimized for volume manufacturing and testing to support the next generations of constellations. The solution features a wide range of telecommands and telemetries providing direct access to the variables that control it for maximum flexibility if additional functionality is required over the initial 3 operation modes offered (Torque, Speed or Direct DAC control).

Durable

Designed and extensively tested for the harshness of space. The Trillian-1 reaction wheel can operate at temperature ranges of -40°C to 85°C at an absolute pressure of 1000 mbar. Each unit is tested to NASA GEVS Acceptance levels prior to shipment ensuring the Trillian-1 can survive a wide range of launch loads, offering flexibility in mission configuration.

Why the TRILLIAN-1?

  • Flown Since 2019
  • Maximum Torque: 47.1 mNm.
  • Maximum Rotation Rate: 6500 rpm.
  • Input filters to reduce signal noise.
  • Total Momentum Storage: ±1.2 Nms.
  • A dedicated motor driver control circuit.
  • Protection Circuitry.
  • 10+ telecommands and telemetries.
  • Low Mass: 1.5 kg.
  • Low Power: 24 W peak.
  • Compact: 135x135x82mm

Related products

ANT-GPS-A
AAC SpaceQuest

ANT-GPS

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
MTQ800 Magnetorquers
AAC Hyperion

MTQ800

The small satellite precision performance MTQ800 magnetorquers enable precise pointing and rapid de-saturation of any reaction wheels in the satellite.
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.

Enquire about this product

"*" indicates required fields

Name*