This course visits the Moon, Mars, the outer planets, and small bodies in the modules ahead — but it starts with Earth on purpose. Every outbound mission has to physically pass through Earth's own space environment first, and Earth is the one planet we can check our answers against. That makes it the natural baseline case for everything that follows.
SSA-01 Module 2 introduced the Van Allen belts. Here's where they sit in the fuller sequence a launch actually passes through.
The lowest ~50 km — where weather happens and nearly all human aviation infrastructure operates. Thin by planetary standards, but where most of a launch vehicle's aerodynamic stress occurs.
A region of charged particles roughly 60–1,000 km up, created by solar radiation stripping electrons from atmospheric atoms. It reflects and refracts radio waves — the reason long-distance radio communication works at all.
Donut-shaped zones of charged particles trapped by Earth's magnetic field — a radiation hazard spacecraft and crews plan around, first introduced in SSA-01 Module 2.
The full region shaped by Earth's magnetic field, extending tens of thousands of kilometers. Its outer boundary, the magnetopause, is where Earth's field pressure balances the incoming solar wind — the actual edge of Earth's protective bubble.
Beyond the magnetopause, a spacecraft is fully exposed to the solar wind and interplanetary radiation environment — no more Earth-provided shielding, for the rest of the journey.
Earth's global magnetic field deflects most incoming solar wind and cosmic radiation, which is why the surface — and most of low Earth orbit — is a relatively survivable environment. That's not automatic for every world. Later modules in this course will keep returning to this baseline directly: the Moon has essentially no global magnetic field of its own (Module 3), and Mars lost most of its ancient one billions of years ago (Module 4) — both facts that shape what those missions actually have to protect against, compared to what Earth handles for free.
Before any destination-specific module, three numbers already constrain what's even possible to build and fly.
A launch vehicle can only lift so much. Structure, propulsion, power, instruments, and shielding all compete for a share of one fixed total — adding mass anywhere means cutting it somewhere else.
Covered in depth in SSA-02 Module 1 — the total velocity change a mission can afford across launch, course corrections, orbit insertion, and any landing. Every destination in this course has its own delta-v price tag.
Covered in SSA-02 Module 3 — how much shielding mass a mission carries against the radiation environment of its specific route and destination. Outside Earth's magnetosphere, that budget only gets more demanding.
Every module ahead — the Moon, Mars, the outer planets, small bodies — is going to ask the same underlying questions this one just asked about Earth: what's the environment, what does it cost to get there and survive, and what can actually be learned once you arrive. Module 2 covers that last question directly — the methods (flybys, orbiters, landers, rovers, sample return) that decide what any mission, anywhere, can actually tell us.
NASA and NOAA public materials on Earth's magnetosphere and space weather, NASA Glenn Research Center spacecraft systems engineering primers on mass budgeting, and ESA educational materials on the near-Earth space environment.
Module 2 covers how missions actually gather data — flybys, orbiters, landers, rovers, and sample return — the methodology that frames every destination module ahead.