The MAI-6000 is a reliable, robust 6U CubeSat Bus designed on our common CubeSat architecture to maximize flexibility, performance capability and cost. Our satellites are designed to meet your mission needs and time frame. 

The MAI-6000 provides users with up to 4,000 cubic centimeters of payload volume as well as a Payload Orbit Average Power (OAP) of 20 W. The cubesat comes equipped with our own flight proven Attitude Determination and Control System the MAI-400 ADACS which is capable of providing 0.01 degree pointing knowledge and 0.1 degree pointing control using our star tracker.


The CubeSat transceiver can be configured to downlink at rates of 2.0 Mbps or more in S-Band using either AES-256 or National Security Agency (NSA) approved Type-1 encryption.


The MAI-6000 also incorporates the MMA HaWK Solar Array, which can provide either a fixed or single-axis gimbaled solar array configuration.


The satellite is compatible with the Planetary Systems Corporation Canisterized Satellite Dispenser (CSD) and can be adapted to other deployers.

  • Data Interfaces: RS-422 Serial Interface, 5 TTL Discrete Interface

  • Payload Oribt Average Power: 20 W

  • Battery: 8 Li-Ion cells =>92 Watt Hours at 14.4 V

  • Payload Power Interface: Switched 3.3 V, 5 V, & 12 V DC Regulated Power Supply

  • Solar Arrays: MMA HaWK or MAI Solar Array (gimbaled or fixed)

  • Attitude Knowledge: 0.01 degree (Star Tracker) or 1 degree (Earth Limb Sensor)

  • Attitude Control: 0.01 degree (Star Tracker) or 1 degree (Earth Limb Sensor)

  • Type of Pointing: Multiple pre-programmed pointing modes


  • Dimensions: 10 x 20 x 30 cm (nominal)

  • System Mass: Up to 16.9 kg (12 kg availablefor payload)

  • Payload Volume: Up to 4U

  • Construction: Machined 7075 and 6061 Aluminum

  • Mission Design Life: 3 years in LEO

  • Orbit Capability: 350-850km, 0-98.8 degree inclined orbit

  • Frequency: S-Band, X-Band, UHF 

  • Downlink: Up to 2.0 Mbps (using S-Band)

  • Encryption: AES-256 or NSA Type-1 available


CubeSat Specifications

The ADACS Experts with 
150 Units Delivered
and over 25 years on orbit
Complete ADACS and ADACS components for CubeSats and Small Spacecraft.
Performance & Reliability
Guidance and Control
Systems for CubeSats and Small Satellites customized to mission requirements.
Adcole Maryland Aerospace's compact guidance and attitude control systems are designed to accommodate a variety of sensor options and combinations. ADACS sensor configuration examples:
  • 2 Star Trackers
  • 1 Star Tracker - 1 Sun Sensor
  • 2 Earth Horizon Sensors

Technical Questions:

Adaptable and Affordable Cube Satellite Bus


  • 4U Payload Volume Available

  • 12 kg Payload Mass Available

  • 20 W Payload Power Available

  • Proven ADACS for Reliable Guidance and Control

MAI-6000 6U CubeSat

Maryland Location:

2145 Priest Bridge Dr, Ste15
Crofton, MD 21114

Telephone: (410) 451-2505
Fax: (410) 451-2507

Massachusetts Location:

669 Forest Street
Marlborough, MA 01752

Telephone: (508) 485-9100
Fax: (508) 481-6142

Start your mission:

Adcole - Established 1957: From the dawn of the space age to the forefront of the New Space Revolution. 

Heritage and mission History 

Reliable, affordable SmallSats, CubeSats , ADACS and New Space components.