
Widely known and used throughout the astrodynamics and aerospace engineering communities, this teaching text was developed at the U.S. Air Force Academy. Completely revised and updated 2018 edition.
Tactical and Strategic Missile Guidance, Seventh Edition https://www.amazon.com/Tactical-Strategic-Missile-Guidance-S...
Tactical missile warheads https://www.amazon.com/Tactical-Warheads-Progress-Astronauti...
Fundamentals of Astrodynamics https://www.amazon.com/Fundamentals-Astrodynamics-Second-Dov...
Here are two favorite readings for anyone willing to delve more into the subject:
Orbital Mechanics for Engineering Students by Howard D. Curtis
https://www.amazon.com/Orbital-Mechanics-Engineering-Student... Fundamentals of Astrodynamics (aka BMW) by Roger R. Bate, Donald D. Mueller, Jerry E. White, William W. Saylor
https://www.amazon.com/Fundamentals-Astrodynamics-Second-Dov...Another great textbook as suggested by musgravepeter in the comments is
Fundamentals of Astrodynamics and Applications by David A. Vallado, Wayne D. McClain
https://www.amazon.com/Fundamentals-Astrodynamics-Applicatio...Then I read a bunch of research papers and more in depth literature. Richard Battin's work for example.
I've been hacking on a two body orbital mechanics library in C with SIMD extensions, and an interactive sandbox with OpenGL. I wrote both from scratch.
Our final project was to program a crude missile defense system. Great book. It's an old one, but I highly recommend it. It's one of the few textbooks I saved from college.
Yes, if you have a source of lift, and you're within the atmosphere, then you can circumnavigate the globe without reaching orbital velocities. A ballistic rocket generally has no significant source of lift and spends nearly all of its time in space.
> Trajectories are shaped like parabolas, not ellipses.
All orbits are conic sections: either an ellipse, hyperbola, or a parabola (the limiting case between the two). But a parabolic or hyperbolic trajectory has escape velocity, whereas only an elliptic trajectory is planet-bound. The apogee of the ellipse is locally approximated well by a parabola, which is why for non-orbital mechanics ballistic trajectories are often modeled by a parabola, but all suborbital trajectories are actually ellipses, not parabolas. If the Earth were flat and the gravity vector were constant, then they would be actual parabolas.
Orbital mechanics is very counterintuitive. I recommend Fundamentals of Astrodynamics if you'd like to learn more, or play KSP rather than FSP.
> Well it's more like a quarter
On this you are correct, the map I looked at deceived me. :)