Mars Resupply Must Be Planned Around 26-Month Launch Windows
Plan Mars inventories, predeployed return hardware, landing capacity, and contingency stocks around launch opportunities that recur roughly every 26 months.
Space exploration technical articles
Clear explanations of the details that shape real programs.
Spaceflight proposals mix settled physics, early engineering, and ambitious forecasts. Read each claim critically, check its assumptions, and compare it with primary sources.
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Plan Mars inventories, predeployed return hardware, landing capacity, and contingency stocks around launch opportunities that recur roughly every 26 months.
Design an optical space-communications link around narrow-beam pointing, cloud and turbulence outages, multiple ground sites, buffering, relays, and RF fallback.
Keep lunar dust from becoming a cabin-wide health and reliability problem with zoning, airlocks, cleaning, filtration, monitoring, and dust-tolerant hardware.
Separate known microgravity risks from the unknown long-term effects of 0.38 g, then compare exercise and rotating artificial-gravity countermeasures.
Evaluate an orbital propellant depot through boiloff, pressure control, low-gravity gauging, chilldown, transfer losses, docking interfaces, and useful throughput.
Design Mars crew procedures for 21–23 minute one-way delays, solar-conjunction outages, local decision authority, onboard expertise, and store-and-forward data.
Interpret a habitat's water-recovery percentage correctly, then account for oxygen, carbon dioxide, waste streams, maintenance, reserves, and make-up supplies.
Choose a lunar south-pole site by trading illumination, terrain, Earth visibility, thermal survival, and travel distance to ice-bearing permanent shadow.