HARDWARE / PRODUCT

DEFIANT Small Satellite Bus

Space Flight Laboratory (SFL)
DEFIANT Small Satellite Bus

Flight-proven 20–35 kg 27U-format bus for HawkEye 360, NorSat-4, and DND Grey Jay missions. Up to 30 kg payload, S/X-Band comms, multiple propulsion options.

Technical specifications

Mass
20–35 kg
Dimensions
300 × 300 × 400–450 mm (27U form factor)
Payload mass
Up to 30 kg
Payload volume
11,000 cm³
Peak power
50–100 W (body + 2 deployable solar wings)
Payload power
45 W @ 40% duty cycle min; 65 W max
Pointing accuracy (mag)
~2°
Pointing accuracy (star tracker)
10–60 arcsec
Propulsion options
Cold gas, resistojet, monopropellant, iodine electric
Communications
UHF/VHF/S-Band/X-Band; 32 kbps–50 Mbps downlink
GPS navigation
5–10 m accuracy
TRL
9 (flight-proven)
Notable missions
NorSat-4, NorSat-TD, HawkEye 360, DND Grey Jay

About

The DEFIANT is SFL’s medium-small satellite bus, bridging the gap between nanosatellites and larger platforms. At 20–35 kg in a 300×300×400-450 mm (27U) form factor, DEFIANT supports demanding Earth observation, RF geolocation, maritime surveillance, and defence missions with a robust payload capacity of up to 30 kg and 11,000 cm³ of payload volume.

Attitude control options span passive (magnetic + fine sun sensors + reaction wheels, ~2° accuracy) to precision (star tracker, 10–60 arcsec), and propulsion options include cold gas, resistojet, monopropellant, and iodine electric. Communications are configurable across UHF/VHF, S-Band, and X-Band at 32 kbps to 50 Mbps downlink. Flight missions include NorSat-4 (AIS + low-light Arctic imaging, January 2025), NorSat-TD (ion propulsion + laser comms demo), HawkEye 360 RF-geolocation cluster, and DND Grey Jay surveillance satellite.

Documentation

No public datasheet yet — request the datasheet / ICD from the supplier.

Source: www.utias-sfl.net ↗