Deuterium-tritium pellets are injected into the reaction chamber and compressed by pulsed magnetic fields (magnetized inertial fusion). Ignition drives charged plasma out through the magnetic nozzle, producing thrust by Newton's third law.
Compare with chemical engine
Live engine telemetry
ModeFusion (MIF)
Specific impulse (Isp)–
Exhaust velocity–
Instantaneous thrust–
Plasma core temp.–
Ignitions so far0
Δv accumulated0 km/s
⚖️ Tsiolkovsky rocket equation
Fusion
Chemical
Isp
–
–
Exhaust vel.
–
–
Propellant frac.
–
–
Mass ratio m₀/mf
–
–
Δv = Isp·g₀·ln(m₀/mf). For the same Δv, the far higher fusion exhaust velocity needs a dramatically smaller propellant mass fraction than a chemical engine.
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