Further Reading: Launch Vehicles

Launch vehicles sit at the meeting point of propulsion, orbital mechanics, and economics, so the best sources span all three. The items below are Tier 1 (canonical works we are confident exist) or Tier 2 (a real, named resource or vehicle document whose exact edition/URL we do not pin down here). For any number you intend to use, go to the operator's current payload user's guide — the one source that is authoritative and current.

Core textbook treatments

Wertz, Everett & Puschell, Space Mission Engineering: The New SMAD. The systems-engineering reference for this whole part. Its chapters on launch systems, launch-site selection, and the mission-to-launch-vehicle matching process are the professional version of §30.6, with the trade-study machinery laid out in full. Tier 1.

Curtis, Orbital Mechanics for Engineering Students — chapters on orbital maneuvers and launch. For the launch-azimuth-to-inclination geometry ($\cos i = \cos\phi\sin\beta$) and the plane-change and transfer-orbit math behind the GEO penalty of §30.3, Curtis gives clean derivations in the same spirit as this chapter. Tier 1.

Sutton & Biblarz, Rocket Propulsion Elements — chapters on launch-vehicle and stage design. The propulsion reference. Its treatment of staging, propellant choice, and vehicle sizing is the "why" behind the family tree of §30.1. Tier 1.

Primary sources — the real numbers

Launch-vehicle payload user's guides (SpaceX, ULA, Arianespace, Rocket Lab, ISRO, and others). Each operator publishes a payload user's guide giving performance curves (payload versus orbit and $C_3$), fairing dimensions, environments, and interfaces. These are the authoritative, current version of Appendix H's ballpark tables — and the document a real mission actually selects against. Tier 2 — real, freely published documents; find the current edition on each operator's site.

NASA Launch Services Program (LSP) and the NASA Launch Vehicle Performance website. NASA maintains performance tools and documentation used to match science payloads to vehicles, including $C_3$ performance for interplanetary missions of exactly the kind in Case Study 2. Tier 2.

On launch operations and the countdown

NASA and range documentation on launch commit criteria and countdown operations. The public accounts of how a launch is polled and committed — built-in holds, terminal count, the GO/NO-GO process — are the grounded version of §30.5, and they connect directly to the mission-control material of Chapter 31. Tier 2.

Watch and play

Scott Manley and Everyday Astronaut (YouTube) — launch-vehicle and launch-operations explainers. Both cover the fleet, reusability, launch-site geography, and countdown operations at exactly this chapter's level, with real launch footage that makes the abstractions concrete. Everyday Astronaut's countdown-narration and vehicle-comparison videos pair especially well with §30.1 and §30.5. Tier 2.

Kerbal Space Program — launch into a target plane and window. Nothing teaches the azimuth-inclination relation and the instantaneous rendezvous window (§30.3–30.4) faster than trying to launch into an existing craft's plane and paying for every degree you miss. Tier 2 — a commercial game.

Suggested order

1. Reread §30.3 and work its azimuth-inclination worked example, then confirm the geometry in Curtis.
2. Open one real payload user's guide (SpaceX's is the most accessible) and find its LEO, GTO, and $C_3$ performance curves — see how Appendix H's single numbers are really whole curves.
3. Watch an Everyday Astronaut or Scott Manley launch-operations video to hear the countdown and GO/NO-GO poll in real time.
4. If you have KSP, launch into the ISS's plane from a low-latitude and a high-latitude site and feel the difference — then reread §30.3 and §30.4.