Jinwu Electric Propulsion System
Hongqing Technology (鸿擎科技)
The Jinwu Electric Propulsion System is Hongqing Technology next-generation argon-fueled electric propulsion platform, developed entirely in-house for commercial LEO satellite applications. It has been validated on orbit with 4,089 ignition cycles and a 100% success rate, accumulating 1,434 km of cumulative orbital maneuver altitude as of June 8, 2026. The system is composed of three […]
Typed specifications4 values
Discloses 2 of 11 fields engineers filter by in this category (category median 3).
- Mass
- 500 g product page
- Propellant
- argon product page
- Feed / tank pressure
- 30 bar min · product page 300 bar max
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 supplier15 lines, in the manufacturer's own wording
- Propellant
- Argon (Ar)
- In-orbit ignition cycles
- 4,089 (verified as of June 8, 2026)
- Ignition success rate
- 100%
- Cumulative orbital maneuver altitude
- 1,434 km
- Supply module - pressure regulation ratio
- >300:1
- Supply module - control method
- PID closed-loop
- Supply module - pressure response time
- <30 s
- Supply module - pressure accuracy
- +/-2%
- Supply module - flow range
- 0-50 sccm
- Supply module - mass
- 500 g
- Power module - power density improvement
- 3-5x vs. previous generation
- Power module - radiation tolerance
- >80 Krad (Si) total dose
- Power module - single event upset protection
- >37.5 MeV
- Thruster module - anode design
- Conical anode swirl flow
- Thruster module - magnetic configuration
- Magnetic lens with permanent magnet anode
About
The Jinwu Electric Propulsion System is Hongqing Technology next-generation argon-fueled electric propulsion platform, developed entirely in-house for commercial LEO satellite applications. It has been validated on orbit with 4,089 ignition cycles and a 100% success rate, accumulating 1,434 km of cumulative orbital maneuver altitude as of June 8, 2026.
The system is composed of three integrated modules: the Electric Propulsion Storage and Supply Module for precision propellant flow control, the Electric Propulsion Power Module for high-efficiency power conversion with radiation hardness, and the Electric Propulsion Thruster Module incorporating advanced magnetic lens and conical anode swirl-flow technologies to minimize electrode erosion and extend operational life.
Compared to legacy propulsion systems, Jinwu offers higher specific impulse, extended lifespan, and lower cost-per-unit-impulse, making it well-suited for mass-production satellite constellations. The thruster uses argon propellant, which is non-toxic, inexpensive, and widely available, simplifying ground handling and reducing launch safety restrictions.
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.