Table 1. Thruster major specification

Property	Specification
Propellant	Butane
Weight	Total wet mass = 802 g for one moduleTotal dry mass = 682 g for one module
Size	Less than 2 U (20 × 10 × 10 cm) of total size
Thrust level	Max 1 mN for each nozzle
Burn duration	Max 300 sec
Total Delta-V	Around 16 m/s (assuming a 10 kg nanosatellite)