TRINITY HET Hall Effect Thruster
Blue Orbit Space Systems
Argon/nitrogen Hall effect thruster of the TRINITY series for small satellites: under 100 mN thrust, up to 1100 s Isp, LEO to GEO.
Key figurescomparable across the catalogue
- Mass
- 2.5 kg
- Power
- 800 W
- Largest dimension
- 115 mm
- Thrust
- 2.5 N
- Specific impulse
- 1,100 s
- Total impulse
- 1,500 N·s
Normalised to common units so this product can be compared with others in its category. The supplier's own wording is below.
As published by the supplier
- Propellant
- Argon, Nitrogen
- Mass (incl. thruster and cathode)
- 2.5 kg
- Dimensions
- 90 x 85 x 115 mm
- Nominal input power
- 800 - 1200 W
- Operational power range
- 1500 W
- Thrust
- < 100 mN
- Specific impulse
- < 1100 s
- Efficiency
- < 50%
- Life
- < 3000 hours
- Total impulse
- < 1500 kN-s
- Nominal flow rate
- 6 mg/s
- On/off cycles
- 5000
- Altitude
- From LEO to GEO
About
The TRINITY HET is the Hall effect thruster of Blue Orbit Space Systems’ TRINITY series, a solution designed for small satellites.
It runs on argon or nitrogen propellant and delivers under 100 mN of thrust at up to 1100 seconds specific impulse, with a total impulse below 1500 kN-s over a life of up to 3000 hours and 5000 on/off cycles. The unit is rated from LEO to GEO altitudes.
The quoted mass of 2.5 kg includes both the thruster and the cathode.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.