Mars Landing Window Simulator Orbital Physics Engine

Simulate Earth-Mars Hohmann/Fast transfers, launch hardware constraints & poll feasibility (2026–2058)

Architecture Presets:
Synodic Launch Window Explorer (26-Month Cycle) Selected Launch: Q3 2033 (Window #4)
Mission Parameters
8 flights
120 tons
2032
$15 Billion
Transfer Delta-V Requirement: 3.90 km/s
Earliest Feasible Landing Achievable
2033 (2030–2039)
Mission Architecture Feasibility Score: 78%
Primary Critical Bottleneck:

Surface ISRU propellant production rate

Poll Options Probability Distribution World of Statistics Sync
This decade (2026–2029) 4%
2030–2039 68%
2040–2049 22%
2050–2059 or later 6%
Selected Mission Timeline Gates Window 2033
Q3 2033
Earth LEO Departure & Trans-Mars Injection (TMI)
Q1 2034
Heliocentric Cruise & Deep-Space Insertion (~180 Days)
Q1 2034
Mars Aerobraking, EDL & First Human Crew Touchdown
Q3 2035
Surface Stay (~500 days) & ISRU Fueled Return Departure
Synodic Opportunities Computed: 2026, 2028, 2031, 2033, 2035, 2038, 2040, 2042
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