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Princeton Fusion Systems

A New Jersey company developing the Princeton Field-Reversed Configuration reactor, a compact device that uses rotating magnetic fields and radio-frequency heating to confine a small, hot plasma for clean fusion energy and space propulsion.

Reviewed Last reviewed: 9 Aug 2026 · Category: Companies & Programs

Origins and Mission

Princeton Fusion Systems (PFS) was founded to commercialize the Princeton Field-Reversed Configuration (PFRC) concept developed by Samuel Cohen at the Princeton Plasma Physics Laboratory (PPPL). The PFRC is a compact magnetic-confinement device that uses odd-parity rotating magnetic fields (RMF) to both form and heat a field-reversed configuration (FRC) plasma. Cohen's research at PPPL dates to the early 2000s, and PFS was established to carry the concept from laboratory experiment toward a practical reactor.1

Key fact: The PFRC-2 experiment at PPPL has demonstrated electron temperatures exceeding 500 eV and ion temperatures above 1 keV in a plasma roughly 20 cm in diameter — remarkably hot for such a small device. The concept aims to reach fusion conditions in a machine small enough to fit in a room.2

Technical Approach

The PFRC uses a field-reversed configuration, a toroidal plasma confined by its own internal currents with no material center post or complex external coil array. What distinguishes Cohen's approach is the heating method: odd-parity rotating magnetic fields preferentially heat electrons, which then transfer energy to ions through collisions. This method avoids the large neutral-beam injectors and high-power microwave systems used in tokamaks.

The ultimate fuel target is deuterium-helium-3 (D-3He), an advanced fuel cycle that produces mostly charged particles rather than neutrons. While D-3He has a higher ignition threshold than deuterium-tritium, the PFRC's compact geometry and efficient heating scheme are designed to reach the required temperatures (tens of keV ion temperature) in a device small enough to be economically attractive.3

The reactor concept envisions a cylindrical vacuum vessel only a few meters long, with superconducting coils providing the external magnetic field. Fusion products — primarily 14.7 MeV protons and 3.6 MeV alpha particles from D-3He — would be captured by direct energy conversion, similar in principle to concepts explored for mirror machines.

Space Propulsion Applications

The PFRC's small size and high specific power make it a candidate for space propulsion. NASA has funded studies of a Direct Fusion Drive (DFD) concept based on the PFRC, in which the fusion exhaust is directed out a magnetic nozzle to produce thrust. Missions studied include rapid transit to Pluto, Jupiter, and Saturn, as well as interstellar-precursor trajectories.4

Dual-use potential: A single PFRC-class reactor could, in principle, provide both thrust and electrical power for a deep-space mission — eliminating the need for separate propulsion and power systems and enabling mission profiles inaccessible to chemical or solar-electric spacecraft.

Current Status

The PFRC-2 experiment continues at PPPL, incrementally increasing plasma parameters. PFS has received funding from NASA, ARPA-E, and the Department of Energy. The next major step is PFRC-3, which would operate with deuterium fuel (rather than the hydrogen and helium gas used in PFRC-2) and aim to demonstrate fusion-relevant ion temperatures. The path from PFRC-2 to a net-energy reactor remains multi-step, but the concept's compactness and fuel flexibility give it a distinctive position in the fusion landscape.5

Sources

  1. Cohen, S. A. et al. Formation of collisionless high-beta plasmas by odd-parity rotating magnetic fields. Physical Review Letters, 98(14), 145002, 2007.
  2. Cohen, S. A. et al. RF heating results in the PFRC-2 device. Bulletin of the American Physical Society, 2019.
  3. Cohen, S. A. et al. The Princeton Field-Reversed Configuration concept for compact fusion power. Journal of Fusion Energy, 36, 126-133, 2017.
  4. Thomas, S. J. et al. Fusion-enabled Pluto orbiter and lander. Journal of Spacecraft and Rockets, 56(3), 2019.
  5. Princeton Fusion Systems. Company overview and PFRC development roadmap. Company website, 2024.

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