Further Reading: Atmospheric Re-Entry

Re-entry sits at the crossroads of orbital mechanics, aerodynamics, and materials science, so the good sources come from all three. The list below is Tier 1 (canonical works we are confident exist) or Tier 2 (a real, named result or resource whose exact edition/page we do not pin down here). Start with the overviews; the primary sources reward a second pass.

Core textbook treatments

Anderson, Hypersonic and High-Temperature Gas Dynamics (AIAA). The standard reference for the physics of §7.2–7.3: shock layers, stagnation-point heating, the blunt-body principle, and real-gas effects (dissociation, ionization). If you want the rigorous version of "why it's compression, not friction," this is the book. Tier 1.

Regan & Anandakrishnan, Dynamics of Atmospheric Re-Entry (AIAA Education Series). A dedicated re-entry text covering the trajectory dynamics, the corridor, and heating in one place — the natural next step after this chapter for the ⭐⭐⭐ material. Tier 1.

Curtis, Orbital Mechanics for Engineering Students. Our orbital-mechanics anchor. Its treatment of the deorbit maneuver and entry trajectory connects §7.1's deorbit burn to the vis-viva tools of Chapter 6. Tier 1.

Wertz, Everett & Puschell, Space Mission Engineering: The New SMAD. The systems view: where entry, descent, and landing (EDL) and thermal-protection sizing fit into mission design, and the mass and margin bookkeeping behind the Mission Design Checkpoint. Tier 1.

The primary sources

Allen & Eggers, "A Study of the Motion and Aerodynamic Heating of Ballistic Missiles Entering the Earth's Atmosphere at High Supersonic Speeds" (NACA Report 1381, 1958). The origin of both the blunt-body insight (§7.2) and the peak-deceleration result (§7.6). Reading even the introduction shows how a single counterintuitive idea — maximize drag to survive — was argued from physics. Tier 1 — a real NACA report; find it via the NASA Technical Reports Server.

Columbia Accident Investigation Board (CAIB) Report, Volume I (2003). The definitive account of how a breach in the reinforced carbon-carbon leading edge let shock-layer gas into Columbia's wing (the §7.3 connection). Volume I is as much about organizational failure as physics, and it is the bridge to Chapter 32 and Chapter 37. Tier 1 — a real government report, freely available.

Sutton & Graves, stagnation-point convective-heating correlation (NASA technical report, early 1970s). The source of the $\dot q \propto \sqrt{\rho/R_n}\,v^3$ scaling used throughout §7.3. Useful if you want to compute an actual heat flux rather than a ratio. Tier 2 — a real, widely used correlation; verify the exact report and constant before quoting a number.

On the vehicles

NASA history resources on the Apollo command module heat shield (AVCOAT) and re-entry. Free, well-illustrated accounts of the ablator, the corridor, and the guided lifting entry that Case Study 1 audits. A good check on this chapter's Apollo numbers. Tier 2 — long-running NASA educational/history pages; search the title for the current URL.

Watch and play

Scott Manley, YouTube — videos on re-entry heating, heat shields, and the blunt-body idea. The clearest short explanations of why capsules are blunt and why they glow, from a genuine expert. Pairs well with §7.2 and §7.4. Tier 2.

Kerbal Space Program (with re-entry heating enabled, stock or the "Deadly Reentry" mod). The fastest way to feel the corridor: enter too steep and you explode; too shallow and you skip back to space; get $\beta$ and the angle right and you land. Everything in §7.4–7.6 becomes tactile. Tier 2 — a commercial game.

Suggested order

1. Reread this chapter's §7.1 (the energy problem) and §7.2 (compression, not friction), then watch Scott Manley on heat shields to hear a second voice on the blunt body.
2. Skim Anderson's opening chapters on shock layers and stagnation heating for the rigorous §7.2–7.3.
3. Read the introduction of Allen & Eggers (NACA 1381) to see the blunt-body argument in the original.
4. Read the executive summary of the CAIB report to ground theme #2 — space is unforgiving — in a real loss, then carry the lesson into Chapters 32 and 37.
5. If you have KSP, fly three re-entries — one too steep, one too shallow, one in the corridor — and then reread §7.5. The corridor will never be abstract again.