Cislunar Orbital Defense & Mission Planner

EPOCH: T+04:12:00 FIELD: EARTH-MOON RESTRICTED 3-BODY PATROL STANCE: HIGH DEFENSE

🎯 Interactive: Click/drag spacecraft or toggle waypoints to simulate orbital transfer maneuvers

Tactical Mission Scenarios USSF Cislunar Ops

Flight Telemetry & Propulsion Audit Validated Engine

Trans-Lunar Injection (TLI)

3.12 km/s

Lunar Orbit Insertion (LOI)

1.03 km/s

Total Delta-V Required

4.15 km/s

Final Dry Mass

3,410 kg

Calculated Wet Mass

18,944 kg

Available Delta-V Cap

7.56 km/s

Orbital Insertion Parameters

Departure Orbit

Destination Target

Payload & Avionics Mass 2,500 kg

Engine Specific Impulse (Isp) 450 s

Propellant Fraction 0.82

Cislunar Delta-V Maneuver Schedule