Dr. Charles Buer (NASA electrostatics physicist) and Andrew Ojima (40-year space program engineer) have developed a fuel-less electrostatic propulsion system through their company Exodus Propulsion Technologies, claiming it can enable continuous acceleration to Mars in 3.5 days using only a car battery’s worth of energy.
The core technology: electrostatic propulsion without propellant
The system generates thrust using only electrostatic fields — no fuel, oxidizer, or expelled mass — by exploiting a higher-order quantum electrodynamics effect that allows net momentum without recoil.
Dr. Buer explains it through third-order perturbation theory: in Coulomb’s law (second order), virtual photon exchange between charges produces equal and opposite recoil so the system’s center of mass doesn’t move; in the third order, an additional virtual photon carries momentum away without being caught, so the whole system translates.
The practical mechanism relies on geometric asymmetry: a small-area high-field region (sharp tips or edges) and a large-area low-field region create unequal electrostatic pressures, producing net force in the direction of the larger area.
The thrust persists after power is removed because charge driven into dielectric materials remains “frozen” and continues generating the field; thrust decays only as charge slowly leaks through imperfect insulators.
They call it the “Star Trek impulse engine” — energy in (electrostatic charge), spaceship moves — but reject “anti-gravity” or “electrogravitics” labels due to fringe connotations.
Why chemical rocketry cannot support a spacefaring civilization
Chemical rockets are fundamentally limited by the rocket equation: Starship is ~95% fuel by mass; geostationary satellites are ~5% payload; most satellite mass is station-keeping propellant.
Mars via chemical propulsion requires 40–50 launches to assemble enough fuel in orbit, 9-month coast, and <1% of initial mass delivered to the surface; return requires manufacturing fuel on Mars.
Ojima, a rocket propulsion specialist, argues chemical rocketry’s realm is low Earth orbit only; reaching the outer planets takes 7–11 years, making it impractical for sustained exploration.
Ion engines improve specific impulse to 3,000–4,000 seconds but remain “chemical engines with an electrostatic punch” — still propellant-limited.
Development history: two decades, a wrong theory, and the asymmetry breakthrough
Ojima spent 20+ years searching for alternatives, initially pursuing field momentum (E×B) thrusters, but discovered hidden momentum (a relativistic counter-effect) cancels thrust when charges flow.
In 2016, Ojima approached Buer with a crude working device; Buer’s wife suggested it matched Buer’s own electrostatic research, leading to collaboration.
They spent two years pursuing a field-momentum theory with static charges (avoiding hidden momentum), building a “giant needle” device at 140 kV that lifted 3–4 feet — but the theory was ultimately wrong.
The breakthrough came when they embedded a thruster in styrofoam, eliminating magnetic fields and current, yet thrust persisted — forcing a return to pure electrostatics and the discovery that geometric asymmetry drives the effect.
Hundreds of “Pac-Man” asymmetric test articles confirmed: thrust scales with area asymmetry, voltage differential, and field strength, not with current or magnetic fields.
Experimental rigor: vacuum, shielding, and answering skeptics
They test in high vacuum (10⁻⁶ torr, harder than Mars surface pressure) inside Faraday-shielded chambers (ITO-coated PET boxes) to eliminate ion wind, Coulomb attraction to surroundings, and Earth’s magnetic field interaction.
Force is measured on the entire shielded box via load cells (digital, automated, no human in loop), not just the internal thruster, ruling out external attraction.
Control tests include: dummy plates without asymmetry (no thrust), polarity reversal (thrust reverses), 180° rotation (thrust follows device), supermagnet underneath (no effect), multiple plastic bag layers (thrust persists).
Molecular water on surfaces initially masked thrust; 12-hour pump-down required for surfaces to dry and thrust to appear — a critical learning for reproducibility.
They have run ~2,500 experiments, with ~3,500 failed designs; current best: 50 millinewtons thrust, over-unity (1.8× device weight), 10⁷ V/m fields (two orders above air breakdown).
Performance claims and near-term applications
50 millinewtons ≈ lifting two sheets of paper on Earth; but in space, continuous thrust accumulates: 1,000 units → 5 N → 38 g continuous acceleration → Mars in 3.5 days (accelerate halfway, flip, decelerate).
Energy requirement: a car battery could power the transit; once static fields form, power can be cut and thrust persists.
First product: CubeSat propulsion module (3U form factor) for station-keeping, orbit raising, and interplanetary transfer — never runs out of propellant, enables constant altitude gain.
CubeSat + propulsion module ~$300k; launch ride $300k–$1M; total ~$1–2M per mission (need two for redundancy); they have potential customers but need space-rating funding.
Long-term vision: ships of any shape (sphere, panel, Borg cube) with propulsion cells stacked for volume or area; 0.5 Earth gravity thrust now, 2.5× lunar gravity, 1.3× Mars gravity — can land/take off from Moon and Mars.
Institutional friction: patents, NASA, and the “poisoned well”
First patent stalled 3.5 years in USPTO (DoD then NASA review); issued only after external reviewers declined due to conflict of interest (they were on the team).
Second patent rejected as “violating conservation of momentum”; they’ve spent years explaining the physics, submitting affidavits and reproduction videos, awaiting resolution.
NASA Kennedy Space Center (Buer’s employer) reacted with indifference: “go away, we don’t care” — partly due to technology transfer “swim lanes” that would force handoff to another center.
Rocket industry skepticism is high: “well has been poisoned” by decades of false propellant-less claims; investors and primes demand escalating proof (vacuum, rotation, float, stackable, etc.).
They are self-funded, part-time until Ojima’s recent retirement; now seeking first customer to fund space qualification rather than waiting for prime contractors or DARPA.
UFO/UAP context and the consciousness question
They distance their work from Tic Tac videos: 10,000 g maneuvers would smear humans and crush known materials; inertia reduction would be required, which a separate APEC researcher claims in early stages.
Bob Lazar’s gravity-wave/Element 115 story: Buer speculates Lazar’s “gravity wave amplifiers” may have been electromagnetic transmitters; the directional movement matches their thrust-vector geometry.
Buer reports a personal 45-minute orb encounter at Cocoa Beach (2013): light undulated 3 miles offshore, brightened to nuclear-flash intensity, helicopters hovered over it, then it approached, split into 5–6 basketball-sized lights, rotated like spokes into breaking waves, followed them, and departed only when he mentally “told it to go away.”
Buer asserts telepathy and clairvoyance are real, learnable skills (tested with family); telekinesis unproven; consciousness interaction with phenomena is an open mystery.
They note Jeffrey Epstein funded consciousness/telepathy research with top scientists (Dean Radin), but warn of background-check necessity.
Space history perspective: Saturn V, Apollo, Artemis
Saturn V had a “pogo” combustion instability (fuel sloshing → pressure oscillations) nearly lost a flight; fixed with simple baffles in first-stage combustors after flight testing revealed it.
Apollo succeeded (6 of 7 landings) because they tested 10,000 times before crewed flights and made only tiny iterative improvements (removing 4 tons of telemetry rings by final mission).
Artemis reuses RS-25 shuttle engines (highest ISP ever, ~450 s) but throws everything away; new methane/oxygen engines reach ~99% theoretical ISP — impressive but still chemical.
NASA has been a “ping-pong ball of politics” since inception: budgets cut, missions canceled, teams rearranged — not how to build sustained capability.
All NASA imagery is public; lunar orbiters have mapped the Moon 20× over, resolving footprints and fallen flags; no hidden cities or cannons.
Asteroid defense: a compelling use case
Current planetary defense: DART mission took 2 years to reach a room-sized asteroid and nudged it with a copper slug — too slow for a 6-month warning.
Exodus system: reach any inner-solar-system object in days, attach thrusters, push continuously — no need to blow it up, just deflect slightly.
Vera Rubin Observatory (Chile) will detect ~20,000 new asteroids daily; if one threatens a city, chemical rockets cannot respond in time; their technology could.
The team and open invitation
Core duo plus 8–10 rotating specialists (electrical, mechanical, materials, modeling, business, high-speed bicycle prototyping).
They publish build videos (e.g., $1.50 “pretzel can” thruster, foam thrusters) so hobbyists can replicate — hoping for “lifter” path to mainstream acceptance.
Peer review will take decades; they won’t wait — hardware that works, reproduces, and survives controls is their standard.
Website: exoduspropulsion.space (under rebuild); they welcome hands-on visitors who sign NDAs.
