Mission Config & Parameters
ORBITAL PROFILE
Target Destination
Mars (6-Month Transit)
$120 Billion
Historical Apollo peaked at ~4% of federal budget ($280B in 2024 USD). Space missions require steady multi-administration capital.
65%
Without geopolitical rivalry (Cold War) or broad public buy-in, multi-year funding dries up as soon as milestones slip.
75%
Closed-loop water and oxygen recovery. If an ECLSS subsystem fails on Moon: 3 days to Earth. On Mars: fatal in transit.
80%
Galactic Cosmic Rays (GCR) and Solar Particle Events (SPE). Interplanetary transit requires massive mass penalties or storm shelters.
Aerospace Engineering Reality: As noted by NASA veterans, the Moon allows abort-to-Earth trajectories within 72 hours. Mars transit is 6 months each way across an unforgiving radiation sea with no emergency abort return.
Simulation Telemetry & Viability
REAL-TIME REEVALUATION
Survival Probability
74%
Calculated via ECLSS & SPE shielding integration
Political Sustainability
Moderate
Congress/public funding stamina over 8-year span
Cost Efficiency Score
B+
Payload capacity to orbit per $B invested
Primary Bottleneck
Radiation Exposure & Transit Time
Critical point of failure limiting human transit
SYSTEM CAPABILITY PROOF TELEMETRY
Target Destination:
mars
Mission Survival Probability:
74%
Mission Viability Status:
Viable Long-Term Transit
Political Sustainability Index:
Moderate
Cost-Efficiency Score:
B+
Identified System Bottleneck:
Radiation Exposure & Transit Time