Rogue
Magdrive
The Magdrive Rogue is an integrated electric propulsion system for 2U CubeSats, utilizing a metal propellant and pulsed power to generate high thrust.
Typed specifications17 values
Discloses 7 of 10 fields engineers filter by in this category (category median 3).
- Propulsion family
- electric ECO · datasheet p.2 electric pulsed plasma thruster | electric SPORT
- Mass
- 3 kg full system · datasheet p.1
- Thrust
- 4 000 mN ECO · datasheet p.2 10 000 mN SPORT | 0.1–10 mN
- Envelope (L×W×H)
- 20 10 10 datasheet p.2
- Specific impulse
- 1 500 s datasheet p.1 4 500 s ECO | 1 800 s SPORT
- Total impulse
- 3 000 N·s min · datasheet p.1
- Propellant
- metal fuel storable solid metal propellant · datasheet p.1
- Power consumption
- 0.2–100 W datasheet p.1
- Power at thrust
- 150 W ECO · datasheet p.2 150 W SPORT
- Thrust vector control
- other magnetic vectoring up to 10° (TBC) · datasheet p.1
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 supplier11 lines, in the manufacturer's own wording
- Integrated system fits inside
- single 2U cubesat
- Dry mass (including propellant, onboard processor, energy storage, and plasma injector)
- 2.5 kg
- Pulsed power system (pps) delivers
- multi-kA, MW class electrical current pulse
- Directional thrust vectoring
- up to 10˚
- Power
- 2 – 100 W
- Thrust
- 0.1 – 10 N
- Specific impulse
- 1500 s
- Total impulse
- >3 kN s
- Energy storage
- 10 kJ
- Mass
- 3 kg
- Dimensions
- 20x10x10 cm
About
The Magdrive Rogue is an advanced electric propulsion system designed for small satellites, specifically fitting within a 2U CubeSat form factor. It generates thrust an order of magnitude higher than other similarly sized electric propulsion systems. The full integrated system has a dry mass of 2.5 kg, which includes the propellant, an onboard processor, energy storage, and a plasma injector. The thruster employs a pulsed power system (PPS) to deliver a multi-kA, MW class electrical current pulse to the plasma injector, creating a high-energy plasma from a metal propellant. This metal propellant eliminates the need for heavy fuel tanks, cryogenics, or pressurization, and removes handling hazards. The system offers customizable performance, allowing for adjustable specific impulse and deep throttling, which is crucial for rendezvous, proximity operations, and precise maneuvering. An integrated microprocessor enables easy integration and command through the satellite’s master controls. Furthermore, the Rogue features directional thrust capabilities, allowing a single thruster to vector up to 10 degrees by altering its magnetic properties, suitable for both main propulsion and attitude control.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.