LM

Lunar Mass Driver & Space Elevator Feasibility Workbench

Vacuum Dynamics & Lagrange Tether Workbench
Presets:
Mission Parameters MASS DRIVER
Target Velocity (v) 2,380 m/s
1.0 km/s (Suborbital) 1.68 (LLO) 2.38 (Escape)
Peak Acceleration (a) 3.5 g
3.5g (Crew Safe) 15g (Rugged) 60g (Regolith)
Payload Mass 5,000 kg
Track Exit Ramp Angle 15°
Lunar Vacuum Advantage: Zero atmosphere allows ground-level orbital ejection at 1,680+ m/s without aerodynamic heating, drag, or sonic shockwaves.
MODE: MASS DRIVER VACUUM TRAJECTORY
STATE: LUNAR ESCAPE (TEI)
APOAPSIS: ESCAPE | PERIAPSIS: SURFACE
Engineering Telemetry REAL-TIME
Track Length 82.52 km
Launch Duration 69.34 s
Kinetic Energy 14.16 GJ
Peak Power 408.4 MW
Orbital Regime Lunar Escape (Trans-Earth Injection)
Human-tolerant acceleration sustained under 3.5g limit; required track length 82.5 km across lunar mare terrain.
Economic Comparison
Chemical Rocket Launch: $3,500 / kg
Electromagnetic Driver: $18 - $45 / kg
L1 Space Elevator: $30 - $70 / kg
Why Moon Elevators Work Today: The Moon's low gravity (1.62 m/s²) means tether tension reaches a peak of only ~3 GPa at L1, perfectly compatible with off-the-shelf Zylon or Kevlar taper ratios (~1.5:1), compared to Earth which requires 60+ GPa taper ratios exceeding 100,000:1.
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