LeoBear — 500 W Hall-Effect Thruster
Pulsar Fusion
Pulsar Fusion's LeoBear is a 500 W Hall-effect thruster for LEO small satellites: 13–36 mN thrust, 1,200–2,300 s Isp on krypton or xenon, 130×130×150 mm, ESA GSTP-funded for TRL 6, with Momentus Vigoride in-orbit demonstration planned for late 2026.
Typed specifications18 values
Discloses 8 of 10 fields engineers filter by in this category (category median 3).
- Propulsion family
- electric datasheet p.2
- Mass
- 3 kg assembly mass · datasheet p.2 3 kg Assembly Mass
- Thrust
- 12–33 mN datasheet p.2
- Envelope (L×W×H)
- 130 x 130 x 150 datasheet p.2 outer diameter 105, height 123; mounting plate 117 x 117 thruster head
- Specific impulse
- 1 300–1 500 s datasheet p.2 2 058–2 300 s
- Total impulse
- 0.87–2.39 N·s datasheet p.2
- Propellant
- xenon datasheet p.5 krypton | argon
- Supply voltage
- 300–400 V datasheet p.2
- Power consumption
- 300–500 W nominal · datasheet p.2
- Thruster technology
- Hall effect datasheet p.2
- Power at thrust
- 300–500 W datasheet p.2
- Random vibration
- 20 g RMS vibration table test, Harwell 2021 · datasheet p.2
- Discharge (anode) voltage
- 300–400 V datasheet p.2
Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.
As published by the supplier10 lines, in the manufacturer's own wording
- Power
- 500 W (tested 296–832 W)
- Thrust (Kr)
- 13–36 mN
- ISP (Kr)
- 1,199–2,149 s
- ISP (Xe)
- 2,058–2,300 s
- Anode efficiency
- Up to 44.8% (Kr); up to 49% (Xe)
- Cathode type
- LaB6 (lanthanum hexaboride)
- Propellants
- Krypton (primary), Xenon
- Dimensions
- 130 × 130 × 150 mm
- TRL
- 3 → 6 (ESA GSTP funded, 18-month program, 2025–2026)
- Flight demo
- Momentus Vigoride OTV, planned late 2026
About
The LeoBear (PF-LEOBEAR) is Pulsar Fusion’s entry-level Hall-effect thruster designed for LEO small satellite applications including orbit raising, station-keeping, and drag compensation. Tested from 296 to 832 W input power, the thruster delivers 13–36 mN thrust at 1,200–2,300 s specific impulse on krypton propellant (and up to 49% anode efficiency on xenon). The LaB6 (lanthanum hexaboride) cathode variant is the primary commercial configuration. Dimensions are 130 × 130 × 150 mm. The European Space Agency selected the LeoBear for a GSTP (General Support Technology Programme) contract in 2025 to advance TRL from 3 to 6 over an 18-month programme. The first orbital demonstration is planned on a Momentus Vigoride orbital transfer vehicle in late 2026. Pulsar Fusion is also developing the 5 kW MoonRanger and 10 kW MarsRanger for higher-energy applications, and the Sunbird nuclear fusion drive as a long-range future programme.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.