Model: 1,000-tonne near-Earth asteroid, 3 km/s capture delta-v, 80 TJ/kg fission energy,
5% burnup, silicate propellant at ~10 MJ/kg effective latent heat. Curves show required
fissile fuel (U-235/Pu-239) as the capture timeline lengthens, accounting for heat loss to
the surrounding rock. Lower-Isp variants consume more rock and lose more energy to conduction.
The dashed green curve adds a photonic wrap + 2,000 m² reflective skirt: free solar-radiation
trim reduces the delta-v the candle must deliver. The dashed gray curves (right axis) show the
free photonic delta-v itself, with and without the skirt — note the units: meters per second.
Photonics is a trim story, not a capture story.
Data generated client-side from the rocket equation. Logarithmic y-axis. Hover for exact values.