Module 1 named two facts about Mars without explaining them: it lost most of its ancient magnetosphere, and a sustained lunar presence is often framed as practice for going there. This module delivers both — plus the specific, concrete reasons Mars missions fail more often than missions to almost anywhere else.
In SSA-05 Module 2's terms — a real climb from lander to rover, one generation at a time.
The first successful Mars landers, running biology experiments that returned genuinely ambiguous results still debated today. Stationary — no mobility at all.
The first Mars rover — Sojourner, small and short-range — proved the "rover" tier of Module 2's methods was achievable on another planet at all.
Far more capable rovers, designed for roughly 90-day missions. Opportunity kept operating for over 14 years — one of the largest planned-vs-actual mission overruns in spaceflight history.
Car-sized, nuclear-powered by an RTG (SSA-01 Module 3), carrying a genuine onboard geochemistry laboratory — a huge jump in what a rover could analyze without ever leaving Mars.
Explicitly built to collect and cache rock samples for a future sample-return mission — actively reaching toward Module 2's hardest tier, not just operating within the rover tier alone.
Radio signals take several minutes to reach Mars, one-way. Landing has to happen fully autonomously — the "seven minutes of terror" during entry, descent, and landing where no human can intervene even if something starts going wrong.
Mars's atmosphere is exactly the wrong thickness — dense enough to demand a heat shield against entry heating, but only about 1% of Earth's density, far too thin for parachutes alone to slow a heavy payload. That gap forces complex, multi-stage landing systems, like Curiosity and Perseverance's rocket-powered sky crane.
Earth and Mars only align for an efficient transfer roughly every 26 months. Missing a window doesn't mean waiting a few weeks — it means waiting more than two years, with real cost consequences for a delayed program.
Module 2 called sample return the rarest of the five methods, and Mars is the clearest case why. Perseverance has been caching samples since 2021 — but caching them is only half the job. Getting a sample off Mars's surface and back to Earth means launching from a real planetary surface with real gravity and a real (if thin) atmosphere to fight through, unlike Hayabusa2's asteroid target (Module 2), where gravity was nearly negligible.
A full Mars Sample Return mission — collect, launch off Mars, and bring material home — has never actually been completed. It remains one of the most technically demanding undertakings in planetary exploration, exactly the kind of cost and difficulty Module 2 predicted for this tier.
Incremental, Moon-First
NASA's stated architecture uses a sustained lunar presence (Module 3) as a proving ground for life support, in-space resource use, and long-duration operations before attempting a crewed Mars mission — a conservative, government-funded timeline.
Direct, Aggressive Timeline
SpaceX has proposed a more direct, Starship-based architecture aimed squarely at Mars, on a far more aggressive announced timeline than NASA's — privately funded, and even less technically validated at Mars scale than NASA's approach.
Neither has flown a crewed Mars mission. Both remain proposals, not demonstrated capability — and both still have to solve the problem Module 1 raised first: without Earth's global magnetosphere, a months-long transit to Mars means real, largely unsolved radiation exposure for any human crew, for the entire trip.
NASA JPL Mars mission pages spanning Viking through Perseverance, NASA Mars Sample Return program materials, and public NASA and SpaceX materials on their respective human Mars mission architectures.
Module 5 covers the outer planets and small bodies — Voyager through New Horizons, and asteroid/comet missions grouped by shared mission profile.