Modules 1 and 2 covered why space is a hard place to build for, and where things end up once they get there. This module is the groundwork for what actually does the building and the getting-there: a lighter overview here, with the deeper engineering treatment waiting in SSA-02.
Casual coverage calls the whole stack "the rocket." Space studies treats them as two separate machines with two separate jobs.
Gets It There
The rocket itself. Its only job is delivering a payload to the right altitude, speed, and trajectory. Most of its own mass — fuel, tanks, boosters — is discarded or burned along the way.
Does the Job
The actual payload. Whatever it was built to do once it's there — orbit Earth, carry a crew, study a planet, dock with a station — happens after the launch vehicle has already finished its part and separated.
Once separation happens, the launch vehicle's story is over — it's re-entering, discarded, or (increasingly) flying itself back down to be reused. Everything from here is the spacecraft's problem: surviving vacuum and radiation, holding the right orbit, and doing whatever it was actually sent up to do.
Regardless of mission, almost every spacecraft is solving the same three problems.
Not just for launch. Once in orbit, propulsion handles station-keeping, attitude changes, and orbit transfers. Chemical thrusters give quick powerful bursts; electric (ion) thrusters sip fuel over much longer burns — a trade-off covered in depth in SSA-02.
Solar panels are the default anywhere near enough to the Sun, with batteries carrying the load through eclipses. Missions heading past Mars — where sunlight gets too weak — often switch to radioisotope generators instead, like Voyager and the Mars rovers.
How a spacecraft knows where it is and points where it needs to. Star trackers and gyroscopes for orientation, GPS in LEO, ground-based tracking farther out, and reaction wheels to turn the vehicle without burning fuel.
No single official cutoff exists — agencies and companies draw the lines differently — but a rough shared framework looks like this:
Built for a single small satellite and a fast, dedicated launch rather than sharing a ride. Rocket Lab's Electron is the clearest example of this class.
The current commercial and government workhorse class. Falcon 9, Soyuz, and Japan's H-IIA all sit here, covering most routine satellite and crew launches.
Reserved for big science payloads and national-security missions that need more mass or more delta-v than a medium-lift vehicle can offer. Falcon Heavy and Delta IV Heavy fall in this range.
Built specifically for crewed lunar and Mars ambitions, and for launching the largest single station or habitat modules. NASA's SLS and SpaceX's Starship both target this class.
The word "spacecraft" covers wildly different machines. What it's for decides almost everything else about how it's built — including which orbital band from Module 2 it ends up in.
Carries People
Life support, abort systems, and return capability are non-negotiable. Missions tend to be shorter than uncrewed ones. Crew Dragon and Soyuz are current examples.
The Bulk of Everything in Orbit
Imaging satellites tend to sit in LEO for resolution; broadcast and weather satellites sit in GEO to stay fixed over one spot on the ground.
Broadcasts a Clock, Not Much Else
GPS and other GNSS constellations live in MEO. Their entire job is transmitting a precise, synchronized time signal that receivers on the ground triangulate.
No Return Trip
Built to travel to other bodies — the Moon, Mars, the outer planets, asteroids — with mission durations that can stretch decades, like Voyager and JAXA's Hayabusa2 asteroid sample-return mission.
Assembled, Not Launched Whole
Long-duration crewed habitats built to dock together in orbit and be resupplied indefinitely rather than replaced — the ISS being the standing example.
Public technical fact sheets from SpaceX, Rocket Lab, ULA, and NASA (SLS/Artemis program pages), plus NASA's power-systems and RTG educational materials.
Module 4 covers space operations, commerce, and resources.