StEP Stellar Electric Propulsion

The End of
Fuel Dependency

StEP is an advanced spaceflight technology that is purely electronic—producing thrust using only solar power, without consuming any form of fuel or propellant.

Stellar Electric Propulsion logo
THE PROBLEM

Traditional propulsion is fundamentally limited

'Old-school' space propulsion engines produce thrust by consuming propellant stored in tanks. Eventually, they empty those fuel tanks.

Even hybrid-electric technologies like ion or plasma engines rely on propellant. When it runs out, the mission ends—regardless of whether objectives have been achieved.

This fundamental limitation constrains every aspect of spacecraft design, mission planning, and operational capability.

Comparison of various ion and plasma propulsion systems

Various ion and plasma engines—all require propellant to function

THE SOLUTION

Propulsion without propellant

StEP thrusters are not hybrid-electric engines. They require no fuel tanks and do not use ion or plasma technology to generate thrust.

Powered by the Sun

StEP gets electric power from photovoltaic arrays. Wherever spacecraft travel, they can use power from the nearest star.

Purely Electronic

Thrust is generated electronically, enabling continuous operation as long as there is access to electric power.

Unlimited Missions

Without fuel constraints, StEP-equipped spacecraft can accelerate, decelerate, and change trajectory indefinitely.

CAD diagram showing StEP spacecraft architecture
PERFORMANCE

Faster, lighter, cheaper

Higher Speeds

Lower spacecraft mass means faster acceleration and deceleration, dramatically reducing transit times.

Shorter Routes

Continuous thrust capability enables direct trajectories rather than fuel-conserving Hohmann transfers.

Lower Costs

Eliminating fuel system mass reduces launch costs. Reusable vehicles multiply the savings.

VALIDATION

Prototype testing ongoing

VSL prototypes have passed several proof-of-concept tests, demonstrating the viability of propellant-free thrust generation.

PROTOTYPE 003

First successful proof-of-concept

The first StEP prototype that passed all of its proof-of-concept tests was code-named '003'. To test it in mid-air neutral buoyancy conditions, we sealed it inside a helium balloon gondola and flew it around our lab.

Watch 003 in flight
Prototype 003 wrapped in thermal insulation Prototype 003 in helium balloon gondola
Prototype 003a operating in vacuum chamber with live telemetry
PROTOTYPE 003a

Smaller, lighter, vacuum-tested

After our successes with 003, we developed thruster '003a'—using the same electronic technology but smaller, lighter, and more tightly engineered than its predecessor.

To validate performance under space-like conditions, we operated 003a inside a vacuum chamber with live telemetry monitoring throttle, vectoring, and system temperature.

Watch vacuum chamber test
APPLICATIONS

Mission capabilities

StEP technology enables missions that are impossible with propellant-dependent systems.

Orbital debris visualization
MISSION 01

Space Debris Mitigation

VSL Space Drones with StEP thrusters will perform multiple missions to Reduce, Reuse, and Recycle dangerous orbital debris.

Earth-crossing asteroid orbital diagram
MISSION 02

Planetary Defense

Intercept and deflect potentially dangerous Earth-crossing objects with the unlimited maneuvering capability of StEP propulsion.

Table of asteroid mining targets and their estimated values
MISSION 03

Asteroid Mining

Survey, mine, and return valuable materials from near-Earth asteroids—enabled by spacecraft that can make the round trip.

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