Station-keeping
Hold the orbit your mission needs, for as long as it needs it.
Small, periodic burns that cancel atmospheric drag and keep the orbit where the mission planned it.
Propulsion
Sized to the mission. Status stated on every part.
Non-toxic propulsion for small satellites, developed around three manoeuvres. Every product below carries its development status, and every figure carries target or measured. Where a number is not yet validated, it is not published.
Product
Thruster
Thruster.STEP · Cycles · studio light · 3q
CADDesign frozen for the first prototype.
Thruster assembly
CAD| Parameter | Value | Basis |
|---|---|---|
| Overall length | 1374 mm | CAD |
| Max. diameter | Ø 408 mm | CAD |
| Parts | 24 | CAD |
| Thrust | — N | target |
| Specific impulse | — s | target |
| Chamber pressure | — bar | target |
Values shown as "—" are pending validation by the engineering team and are not published.
Drawings
From the model, not from an illustration
Every figure is projected from the delivered STEP file by hidden-line removal. Same geometry as the renders, in drawing-office form.
Part
Thruster, elevation
Status
CAD · rev. 1
Scale
NTS
Date
2026-09
Source
Thruster.STEP
Part
Thruster, exploded
Status
CAD · rev. 1
Scale
NTS
Date
2026-09
Source
Thruster.STEP
Applications
Three manoeuvres, one hardware line
Orbit transfer
Move between orbits after deployment, up or down.
Two burns: one to leave the injection orbit, one to circularise at the target.
Deorbiting
Bring the satellite down at end of life and leave nothing behind.
A retrograde burn that lowers the perigee until re-entry, within the 5-year rule.
Next step
Send us the mission envelope.
Orbit, spacecraft mass, available power and the Δv you need. We size against it and come back with what fits and what does not.
Request a proposal →