An aerospace engineer rarely stays inside one subfield for long. A structures specialist is asked to sanity-check a propulsion number. A student sizing a wing spar in one course is expected, a semester later, to reconcile that same structure against an orbital mass budget. The tools for that kind of cross-discipline thinking are usually scattered across a shelf of separate textbooks, each deep in its own corner and largely silent about how it connects to the rest.
Most available material forces a choice between two unsatisfying extremes: a narrow, rigorously derived textbook confined to one subfield, or a broad survey that touches every topic but cannot be trusted for a real calculation. Neither shows how a change in an aerodynamic assumption ripples into a structural margin, a propulsion trade, or an orbital budget, which is exactly the kind of connected reasoning that real vehicle design demands.
This handbook works to close that gap. It derives the governing relations of every core aerospace subfield from first principles, walks each one through complete worked numerical examples with every unit tracked, and returns again and again to how the disciplines actually trade off against one another when a real vehicle is being designed.
Inside, you will:
- Follow the full derivation behind each governing relation in aerodynamics, propulsion, structures, flight mechanics, and orbital mechanics, rather than being handed a formula to memorize.
- Work through complete numerical examples with units tracked at every step, so the arithmetic behind a design number is never left as an exercise for the reader.
- See how mass budgets, power budgets, and cost estimates connect the separate subsystem chapters into a single whole-vehicle view, using the same trade-study methodology a design organization would apply.
- Practice with boxed-answer problems that carry fully justified solutions, useful for checking your own reasoning rather than just your final number.
- Move between atmospheric flight and orbital mechanics inside one connected text, instead of switching between an aircraft-focused book and a separate astronautics text.
- Use the book as a working reference outside your own specialty, with consistent notation established once and cross-references linking every chapter forward and backward to the material it depends on.
Coverage spans the systems engineering design process and the standard atmosphere; subsonic and compressible aerodynamics; aircraft performance and flight mechanics; flight control systems and avionics; structural loads, materials, and damage tolerance; gas turbine and rocket propulsion; orbital mechanics and astrodynamics; spacecraft systems engineering; attitude determination and control; and whole-vehicle design methodology, including mass and power budgeting, trade studies, and conceptual cost estimation.
Written for engineering students who have completed a standard fundamentals sequence, statics, dynamics, calculus through ordinary differential equations, and an introductory fluid mechanics or thermodynamics course, and are ready for aerospace-specific material built on that foundation. It is equally suited to practicing engineers who specialize in one subsystem and need a rigorous, well-derived reference for the subsystems outside their own expertise.
Take the next step toward a connected understanding of how an aerospace vehicle is actually designed, from the atmosphere to orbit. Add this reference to your library and start working through the derivations, examples, and trade-offs that tie the discipline together.
