Engineers inspecting massive superconducting fusion reactor magnet coils with plasma glow
Superconducting magnets generating 351,000-gauss fields now make fusion propulsion feasible

By 2030, the first practical fusion reactor will likely connect to a power grid, marking humanity's transition from burning dead plants to harnessing stellar fire. Yet the most profound implication of this energy revolution won't be cleaner electricity—it will be our first realistic pathway to the stars. Scientists have long theorized that fusion propulsion could accelerate a spacecraft to one-tenth the speed of light, fast enough to reach Alpha Centauri in about 43 years. Recent breakthroughs in magnetic confinement, pulsed fusion systems, and AI-driven plasma diagnostics are transforming this vision from science fiction into engineering challenge.

The Breakthrough: Fusion Technology Reaches Critical Milestones

Three converging developments have fundamentally changed the calculus of interstellar travel. First, China's Institute of Plasma Physics generated a sustained magnetic field of 351,000 gauss—over 700,000 times Earth's natural field—using hybrid superconducting magnets that maintained stability for 30 minutes. This field strength approaches what's theoretically needed to confine fusion plasma hot enough for propulsion-grade exhaust velocities.

Second, the National Ignition Facility achieved net energy gain in 2022, with fusion reactions releasing more energy than the lasers supplied—a Q-factor exceeding 4. While the facility's overall Q-engineering (grid power in versus fusion power out) remains at 0.01, the plasma physics barrier has been breached. Meanwhile, magnetic confinement experiments at JET and newer tokamaks have sustained fusion reactions for nearly a minute, with France's CEA projecting several-hour durations within reach.

Third, Princeton researchers unveiled Diag2Diag, an AI system that synthesizes missing plasma diagnostics from existing sensors. Trained on data from the DIII-D National Fusion Facility, it can predict what broken or absent instruments would measure, reducing reactor mass and complexity—critical factors for spacecraft where every kilogram counts. Together, these advances suggest fusion propulsion has crossed from theoretical possibility to tractable engineering problem.

Historical Context: From Chemical Rockets to Nuclear Dreams

Humanity's propulsion timeline reveals an exponential pattern. Chemical rockets, perfected in the mid-20th century, deliver exhaust velocities around 4.5 kilometers per second—barely 0.0015% of light speed. Nuclear thermal designs like NERVA, tested in the 1960s, doubled that by heating hydrogen through fission reactors. The Centrifugal Nuclear Thermal Rocket (CNTR) now under NASA study promises to double nuclear performance again by spinning liquid uranium, quadrupling chemical rocket efficiency.

Yet even these advanced fission concepts hit fundamental limits. Chemical bonds release electron-volts per reaction; fission releases millions of electron-volts; fusion releases orders of magnitude more. One ton of deuterium contains energy equivalent to 29 billion tons of coal. This density advantage explains why Project Daedalus, a 1970s British Interplanetary Society study, envisioned fusion pulse engines reaching 12% of light speed for missions to nearby stars.

The difference between chemical and fusion propulsion mirrors the gap between sailing ships and jet aircraft—not incremental improvement but categorical transformation. Just as early explorers couldn't cross the Pacific in reasonable timeframes, chemical rockets make interstellar travel absurdly impractical. Alpha Centauri lies 4.37 light-years away; a Voyager-speed probe would take 73,000 years. At 10% light speed, the journey shrinks to 43 years—within a human working lifetime.

Understanding Fusion Propulsion Physics

Fusion rockets work by heating propellant to temperatures where atomic nuclei overcome electromagnetic repulsion and fuse, releasing tremendous energy. The most accessible reaction combines deuterium and tritium (D-T), yielding helium-4, a high-energy neutron, and 17.6 million electron-volts per fusion event. This occurs at approximately 100 million degrees Celsius—six times hotter than the Sun's core.

The engineering challenge is threefold: achieving fusion conditions, sustaining them long enough to extract net energy, and directing the energy into thrust. Magnetic confinement uses powerful magnetic fields to bottle the ultra-hot plasma away from physical walls that would instantly vaporize. The International Thermonuclear Experimental Reactor (ITER), now under construction in France, aims for a Q-factor of 10—converting 50 megawatts of heating power into 500 megawatts of fusion output. ITER's tokamak design uses toroidal field coils in a doughnut shape, with magnetic fields so intense they could levitate an aircraft carrier.

For propulsion, the fusion plasma must be exhausted through a magnetic nozzle rather than contained indefinitely. This nozzle channels charged particles into a directed jet, much as a rocket nozzle shapes combustion gases. The exhaust velocity determines specific impulse—how efficiently propellant converts to thrust. Chemical rockets achieve 4-5 km/s exhaust velocity; fusion concepts aim for 1,000-10,000 km/s or more, approaching 3% of light speed in extreme designs.

Conceptual fusion-powered spacecraft with extensive radiator panels for heat rejection in deep space
Fusion spacecraft require massive radiator surfaces to dissipate waste heat during acceleration

Reaching 10% of light speed (30,000 km/s) requires accelerating a spacecraft to velocities where classical physics still applies but engineering becomes extraordinarily demanding. At 0.1c, the Lorentz factor γ equals 1.005, meaning relativistic effects like time dilation remain negligible at just 0.5%. The kinetic energy per kilogram reaches 4.5 × 10^14 joules—equivalent to about 108 tons of TNT per kilogram of spacecraft. Thermodynamic losses mean the fusion system must generate at least three times this energy, with two-thirds becoming waste heat.

Managing the Thermal Hell: Radiative Challenges

This leads to fusion propulsion's most underappreciated constraint: heat rejection. Accelerating one kilogram to 0.1c over, say, 50 years of continuous thrust generates 5.7 kilowatts of parasitic heat that must radiate into space. The Stefan-Boltzmann law dictates that a surface at 700 Kelvin emits about 13.6 kilowatts per square meter. Therefore each kilogram requires 0.42 square meters of radiative surface.

A 1,000-ton crewed starship—modest by interplanetary standards—would need 420,000 square meters of radiator surface, equivalent to a sphere 75 meters in diameter. This explains why realistic starship designs converge on thin, expansive structures resembling soap bubbles rather than the compact vessels of science fiction. The radiator dominates spacecraft architecture, not the fusion reactor or crew habitat.

Helion Energy's approach sidesteps some thermal management challenges through pulsed operation. Rather than sustaining continuous fusion, their system fires plasma rings at each other at a million miles per hour, generating fusion bursts lasting milliseconds. Their sixth prototype, Trenta, reached temperatures above 100 million degrees Celsius in 2021. The seventh, Polaris, incorporates faster pulse rates and energy-recovery systems, storing over 50 megajoules. Pulsed designs allow brief, intense fusion without requiring long-duration plasma confinement—potentially simpler engineering for propulsion than for stationary power plants.

Helion uses deuterium and helium-3 (D-He3) fuel, which produces fewer neutrons than D-T reactions. While D-T releases 80% of energy as high-energy neutrons requiring heavy shielding, D-He3 releases most energy as charged particles that magnetic fields can direct. This aneutronic advantage reduces radiation damage and simplifies thrust vector control, though D-He3 requires 38 times better plasma confinement than D-T. Helion plans to produce helium-3 through deuterium-deuterium reactions and short-lived tritium decay, creating a closed fuel cycle.

From Laboratory to Spacecraft: Engineering the Transition

Translating terrestrial fusion reactors into propulsion systems requires reimagining nearly every component for space constraints. ITER weighs thousands of tons and relies on massive superconducting magnets, thick neutron shielding, and elaborate cooling systems. A fusion rocket must achieve comparable performance at perhaps 1% of the mass while enduring acceleration forces, vacuum, cosmic radiation, and decades without maintenance.

Recent superconducting magnet breakthroughs offer a path forward. MIT's Plasma Science and Fusion Center, collaborating with Commonwealth Fusion Systems, built the world's strongest fusion magnet using high-temperature superconductors (HTS). These materials enable smaller, lighter magnets producing greater field strengths than conventional low-temperature superconductors. China's 351,000-gauss achievement combined HTS insert coils with low-temperature outer magnets in a hybrid design that maintained stability under extreme conditions, operating continuously for 30 minutes at 35.1 tesla.

AI-driven diagnostic systems reduce another mass penalty. Traditional fusion experiments bristle with hundreds of sensors monitoring plasma temperature, density, and stability. Diag2Diag demonstrates that machine learning can synthesize missing measurements from available data, potentially cutting diagnostic hardware by half or more. For a spacecraft, fewer sensors mean lower mass, reduced power consumption, and enhanced reliability—critical for missions measured in decades rather than laboratory pulse cycles.

Precision engineering at micrometre tolerances, essential for ITER's one-million-part assembly, translates directly to fusion rocket fabrication demands. Magnetic coils must align with sub-millimetre accuracy to avoid plasma instabilities. Helion's Polaris integrates thousands of diagnostics to validate performance across multiple fuel cycles, demonstrating the systems integration maturity needed for space applications.

Fuel Selection: Trading Performance Against Complexity

The choice of fusion fuel profoundly shapes mission architecture. Deuterium-tritium offers the lowest ignition temperature and highest reactivity, making it the near-term baseline. However, tritium is radioactive with a 12.3-year half-life, requiring production through lithium blankets surrounding the reactor. D-T's 80% neutron energy fraction demands heavy shielding, contributing to spacecraft mass and inducing material activation over time.

Deuterium-deuterium reactions eliminate tritium scarcity but require 38 times better plasma confinement and still produce neutrons, though fewer. The reaction yields either helium-3 plus a neutron or tritium plus a proton, with subsequent reactions potentially consuming these products. D-D's advantage lies in fuel availability—deuterium comprises 0.015% of ocean water, essentially limitless.

Proton-boron-11 (p-B11) represents the aneutronic holy grail: fusion without primary neutron production. The reaction yields three helium-4 nuclei (alpha particles) and no radiation, eliminating shielding mass and radioactive waste. Direct energy conversion from charged particles could achieve 85% efficiency versus the 30-40% typical of thermal cycles. The catch: p-B11 requires triple-product conditions 500 times more demanding than D-T, making ignition "highly unlikely with current technology," according to fusion researchers. Experimental flying-car fusion concepts cite p-B11's clean energy profile, but practical spacecraft designs will likely start with D-T or D-He3.

Helium-3's terrestrial scarcity poses supply challenges—Earth's atmosphere contains perhaps 35,000 kilograms total. The Moon's regolith, however, holds an estimated one million tons of He-3 implanted by solar wind over billions of years. Future Lagrange-point space factories could extract He-3 from lunar material, positioning it as a long-term interplanetary and interstellar fuel. Each D-He3 fusion releases 18.3 million electron-volts, with most energy in charged particles rather than neutrons.

Mission Profiles: Reaching 0.1c and Beyond

Accelerating to 10% light speed demands enormous energy and propellant. The rocket equation governs all reaction-drive spacecraft: final velocity depends on exhaust velocity and the natural logarithm of the mass ratio (initial mass divided by final mass). For a fusion rocket with 1,000 km/s exhaust velocity to reach 30,000 km/s requires a mass ratio of e^30, or approximately 10^13—physically impossible.

This is where multi-stage designs, in-flight refueling, or external power sources become essential. Project Daedalus envisioned a two-stage vehicle using helium-3 mined from Jupiter's atmosphere, with pellet-based inertial confinement fusion producing exhaust velocities around 10,000 km/s. Even then, the spacecraft would be mostly fuel, with payload comprising a tiny fraction of departure mass.

Alternatively, beamed energy from massive laser arrays or microwave transmitters in the solar system could power the fusion reactor, allowing propellant mass to be minimized. The spacecraft would use fusion primarily as a high-efficiency thruster rather than energy source, similar to how electric propulsion systems use solar panels or nuclear reactors to ionize and accelerate propellant. Such hybrid architectures blur the line between laser sails and fusion rockets.

Acceleration timelines span years to decades. Accelerating a 1,000-ton craft at one-hundredth of Earth gravity (0.098 m/s²) for 10 years achieves 0.1c, assuming perfect efficiency. Lower acceleration extends the timeline but reduces structural loads and power requirements. Deceleration demands an equal performance budget unless the mission is a flyby, meaning round-trip missions to nearby stars require double the energy and propellant of one-way journeys.

At 0.1c, time dilation remains minimal—just 0.5%—so mission planners need not worry about relativity's stranger effects. A 43-year transit to Alpha Centauri would elapse as 42.8 years aboard ship. However, interstellar medium impacts become significant: colliding with hydrogen atoms at 30,000 km/s imparts energies equivalent to particle accelerator beams, requiring forward shielding against erosion and crew radiation exposure.

Societal Transformation: What Fusion Propulsion Enables

Fusion rockets don't merely make existing missions faster—they unlock entirely new categories of human activity in space. Crewed Mars missions shrink from 2.5-3 year round-trips to 420 days with CNTR fission designs; fusion could further compress this to under a year, slashing astronaut radiation exposure and psychological strain. "The longer you are in space, the more susceptible you are to all types of health risks," notes Dean Wang of Ohio State University, who leads CNTR research. "So if we can make that any shorter, it'd be very beneficial."

Outer solar system exploration transforms from multi-decade odysseys to manageable campaigns. Current chemical propulsion requires gravitational assists and years-long cruise phases to reach Jupiter or Saturn; fusion enables direct trajectories measured in months. Mining operations in the asteroid belt or helium-3 extraction from gas giants become economically viable when transit times don't exceed terrestrial industrial cycles.

Mission control team monitoring first fusion-powered interstellar spacecraft to Alpha Centauri
Fusion propulsion could enable 43-year missions to Alpha Centauri within a single human lifetime

The asteroid belt, Kuiper belt, and Oort cloud—collectively containing millions of objects—transition from distant curiosities to accessible resources and outposts. Fusion-powered tugs could redirect asteroids for mining or planetary defense without decade-long lead times. Stations at Earth-Sun Lagrange points, proposed for space manufacturing, could be supplied regularly rather than annually.

Interstellar missions evolve from generation ships to career commitments. A 43-year mission to Alpha Centauri fits within a professional astronaut's working life, with crews potentially returning before their grandchildren retire. Multi-generational arks remain options for more distant targets, but fusion propulsion offers the first plausible path to sending humans to another star and receiving their findings within a single human lifetime.

Opportunities and Positive Disruptions

Fusion propulsion's development drives breakthroughs across multiple domains. Superconducting magnet technology, essential for plasma confinement, advances power transmission, medical MRI systems, and particle physics research. AI-driven diagnostic systems developed for fusion reactors enhance spacecraft autonomy, robotic surgery precision, and industrial process control—anywhere sensors can fail or coverage is incomplete.

The energy density advantage positions fusion as the ultimate portable power source for space infrastructure. Orbital factories, lunar bases, and Mars settlements could operate fusion plants sized for local needs rather than relying on solar panels with day-night cycles or radioisotope generators with watt-scale outputs. Helion's agreement to supply Microsoft with 50+ megawatts by 2028 marks the first commercial fusion power purchase, signaling investor confidence in near-term viability.

Space-based fusion plants at Lagrange points, processing lunar helium-3, could eventually beam power to Earth or in-space manufacturing complexes, creating an energy economy extending beyond Earth's atmosphere. Fusion's cleanliness—deuterium fuel from seawater, helium as the waste product—eliminates the fission-related concerns of orbital nuclear reactors, making regulatory approval and public acceptance more attainable.

Educational and workforce implications are profound. The International Thermonuclear Experimental Reactor project employs thousands across 35 partner nations, building expertise in plasma physics, superconducting systems, precision manufacturing, and international scientific collaboration. George Tynan, transitioning from aerospace to fusion research at UC San Diego, exemplifies the cross-pollination: "As a potential energy source, it could really be transformative, and the idea that I could work on something that could have that kind of impact on the future was really attractive to me."

Challenges and Risks: The Reality Check

Despite recent progress, fusion propulsion remains unproven engineering. ITER won't achieve first plasma until at least 2025 and full deuterium-tritium operations not until the 2030s. Commonwealth Fusion Systems aims for a 400-megawatt Virginia plant in the early 2030s; Helion targets 2028 for its Washington State facility. Even if these succeed on schedule, a terrestrial power plant differs radically from a space propulsion system.

Mass and miniaturization challenges are formidable. ITER's tokamak measures 28 meters tall and weighs thousands of tons; a fusion rocket must achieve comparable performance at perhaps 100 tons total spacecraft mass to avoid unrealistic propellant requirements. Helion's Polaris at 19 meters long represents progress toward compactness, but it's designed for stationary operation with grid-supplied startup power, not spacecraft constraints.

Neutron radiation from D-T fuel damages materials over time, causing embrittlement and swelling that degrade structural integrity. While p-B11 promises aneutronic operation, its 500-fold increase in required confinement performance relegates it to long-term research. D-He3 reduces but doesn't eliminate neutrons, and helium-3's scarcity demands lunar mining infrastructure that won't exist for decades.

Plasma instabilities remain incompletely understood. Magnetic confinement reactors experience disruptions—sudden loss of plasma confinement—that can damage reactor walls and quench superconducting magnets. Recent AI systems predict disruptions milliseconds in advance, enabling preventive action, but a disruption in a fusion rocket during powered flight could be catastrophic. The engineering margin between stable thrust and mission-ending failure remains uncertain.

Cost represents perhaps the steepest barrier. ITER's budget exceeds $25 billion; developing a fusion rocket would require comparable investment without clear commercial payoff. Unlike fusion power plants that sell electricity, interstellar propulsion serves scientific exploration and long-term survival—goals less attractive to private capital than quarterly returns. Government programs drove chemical and fission rocket development, and fusion propulsion will likely demand similar public commitment spanning decades.

Global Perspectives: International Cooperation and Competition

Fusion research epitomizes both international cooperation and strategic competition. ITER unites 35 nations—including the US, EU, China, Russia, Japan, India, and South Korea—in what participants call a "human adventure" transcending geopolitical disputes. Sabina Griffith, ITER's communication officer, describes seeing delegates from rival nations "standing proudly next to each other" at project milestones.

Yet national fusion programs also reflect great-power competition. China's record 351,000-gauss magnet achievement and sustained plasma confinement experiments position it as a fusion leader, with state media framing breakthroughs as evidence of technological superiority. The US Department of Energy's National Ignition Facility emphasizes American preeminence in inertial confinement, while MIT's PSFC and Commonwealth Fusion Systems pursue private-sector alternatives to international megaprojects.

The fusion propulsion race resembles the mid-20th century space race in strategic implications. Nations achieving practical fusion rockets would dominate solar system resource exploitation, asteroid mining, and off-world settlement—21st-century equivalents of colonial-era sea power. Unlike purely terrestrial technologies, space propulsion inherently advantages first movers through resource access and infrastructure positioning.

Developing countries risk exclusion from fusion benefits. Advanced superconductors, precision manufacturing, and plasma physics expertise concentrate in wealthy nations. Helium-3 lunar mining or Lagrange-point space factories won't be built by nations lacking orbital launch capability. International frameworks ensuring fusion technology sharing—analogous to nuclear non-proliferation treaties—may become necessary to prevent a new axis of technological inequality.

Cultural attitudes toward fusion vary. European public opposition to nuclear power, rooted in Chernobyl and Fukushima memories, complicates fusion acceptance despite its fundamental safety advantages. Asian nations, facing energy scarcity and climate pressure, embrace fusion more enthusiastically. The US balances private innovation culture against declining federal science funding, creating an ecosystem where billionaire-backed startups like Helion coexist with DOE national laboratories.

Preparing for a Fusion Future: Skills and Adaptation

The fusion economy will demand new skill combinations. Plasma physicists who understand magnetohydrodynamics and fusion kinetics remain scarce, with educational pipelines only now expanding in response to private-sector hiring. Superconducting materials engineers, cryogenic systems specialists, and high-precision manufacturing technicians—roles overlapping aerospace, particle physics, and industrial sectors—will be in high demand.

Software engineers specializing in real-time control systems and AI-driven diagnostics are essential. Fusion reactions occur on millisecond timescales, requiring autonomous decision-making faster than human operators. Quantum neural networks, referenced in speculative fusion propulsion concepts, may eventually enable zero-latency critical signal processing, though practical implementations remain experimental.

Systems engineers capable of integrating million-part assemblies with micrometre tolerances across international teams will command premium salaries. ITER's workforce spans dozens of languages and technical traditions, requiring cross-cultural collaboration skills as much as engineering expertise. Space fusion propulsion will add orbital mechanics, astrodynamics, and long-duration mission design to the required knowledge base.

Policy and regulatory expertise is equally critical. Existing space law, largely unchanged since the 1967 Outer Space Treaty, inadequately addresses fusion propulsion, space mining, and interstellar missions. Who owns helium-3 extracted from the Moon? What emissions standards apply to fusion exhausts in cislunar space? How do we prevent weaponization of technologies capable of accelerating payloads to relativistic speeds?

For individuals, positioning for the fusion economy means pursuing interdisciplinary education combining physics, engineering, computer science, and systems thinking. Universities are establishing fusion-specific degree programs; MIT, Princeton, and UC San Diego offer graduate concentrations in plasma science and fusion energy. Online courses in plasma physics, magnetohydrodynamics, and superconducting systems provide accessible entry points.

Investors and entrepreneurs should monitor private fusion companies' progress toward demonstration plants. Helion's Microsoft partnership, Commonwealth's utility agreements, and other commercial commitments signal approaching viability. Adjacent opportunities exist in superconducting materials, radiation-hard electronics, space manufacturing, and cryogenic systems—technologies fusion propulsion will require.

Timeline and Feasibility: When Will This Happen?

Near-term (2025-2035): Terrestrial fusion demonstration plants achieve sustained net energy gain. ITER reaches Q=10; Helion, Commonwealth, and other private ventures demonstrate commercial-scale electricity generation. Superconducting magnet performance improves through HTS material advances. AI diagnostic systems mature, reducing reactor complexity and cost.

Mid-term (2035-2050): First fusion propulsion experiments in orbit, likely scaled demonstrations using simplified fuel cycles. Lunar helium-3 extraction begins via robotic systems supporting cislunar infrastructure. Crewed Mars missions employ fusion-electric hybrid propulsion, proving technologies for deeper space applications. International frameworks establish fusion propulsion standards and safety protocols.

Long-term (2050-2075): Operational fusion rockets enable crewed missions to outer solar system. Interstellar precursor missions—heavily instrumented probes sent to 100+ AU—test sustained high-velocity operation and communications. Multi-decade preparations begin for crewed Alpha Centauri mission, involving fusion propulsion development, closed-loop life support validation, and interstellar trajectory optimization.

Far-future (2075-2100): Crewed interstellar mission launches, targeting 0.1c cruise velocity for ~43-year transit to Alpha Centauri. Mission profile likely includes extended acceleration and deceleration phases, heavy radiation shielding, and multi-generational backup plans despite single-lifetime mission duration. Success opens era of interstellar exploration with fusion propulsion as enabling technology.

These timelines assume sustained funding, absence of major technical showstoppers, and international cooperation—none guaranteed. Fusion energy itself has famously been "30 years away" for 70 years. Recent breakthroughs distinguish the current moment, but translating laboratory success to operational power plants, then to space propulsion systems, involves compounding uncertainties.

Patrick White of the Clean Air Task Force notes utility companies "get a little more serious about their siting and deployment plans, no longer just making vague promises about getting fusion onto the grid 'in a few years.'" This commercial seriousness, backed by Microsoft's Helion contract and utility commitments to Commonwealth's Virginia plant, suggests fusion power's transition from research project to industrial reality is underway.

Fusion propulsion remains a step beyond, requiring space-qualified systems, miniaturization, and performance margins terrestrial plants need not achieve. Yet history shows aerospace technology often advances faster than ground infrastructure once priority and resources align—witness the 1960s Apollo program achieving lunar landings before fusion researchers managed sustained breakeven. If fusion propulsion receives comparable commitment, 0.1c spacecraft could fly within this century.

Conclusion: Betting on Stellar Fire

The convergence of 351,000-gauss magnetic fields, AI-synthesized plasma diagnostics, and repeatedly demonstrated net energy gain marks fusion propulsion's emergence from theoretical possibility to engineering frontier. While formidable challenges remain—miniaturization, neutron management, long-duration reliability—the physics barriers have fallen. What remains is engineering execution, requiring decades of investment and international collaboration.

Reaching 10% of light speed would compress the cosmos from inconceivable to challenging. Alpha Centauri transitions from a point of light to a destination reachable within a career. The thousand nearest stars become a catalog of possibilities rather than merely astronomical data. Humanity's expansion beyond Earth—from tentative orbital steps to Martian settlements to interstellar diaspora—hinges on breakthroughs like fusion propulsion.

The deeper implications extend beyond transportation. Fusion mastery positions civilization to transcend resource scarcity, harness energy rivaling natural processes, and achieve permanence beyond a single planet's fate. Just as fire separated early humans from other primates, fusion may separate spacefaring civilizations from those confined to origin worlds.

Dr. Alain Becoulet, ITER's chief scientist, describes the project as "creating a Sun here on planet Earth." Fusion propulsion aims even higher—bottling a star's power, mounting it on a spacecraft, and riding the exhaust toward other stars. Whether this dream manifests in our lifetimes or our grandchildren's, the pursuit itself advances humanity's capabilities and expands our collective imagination of what's possible.

The question is no longer whether fusion propulsion can theoretically reach 10% of light speed, but whether we'll commit the resources and decades of patient work to make theory real. The answer will determine whether future historians record the 21st century as the era humanity took its first steps toward the stars, or merely the era we calculated how we might, someday, if we chose to try.

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