dc.description.abstract | This textbook is about all basic physical aspects of spaceflight. Not all have been
covered in the past editions. So, what is new in this third edition? First, there are
new sections covering new topics, such as
– Sections 1.2 and 1.3 dealing with the physics of a jet engine and general rocket
performance have been widely extended to more sophisticated effects.
– Sections 7.4.5 and 7.4.6 describe two general solutions to Newton’s gravitational
equation of motion.
– Section 7.7 studies stellar orbits, which are not subject to the standard but more
general types of gravitational potentials.
– Hypersonic flow theory for reentry vehicles is expounded in Sect. 6.2 as a basis
to understand how lift and drag come about and in particular how both depend
on the angle of attack, the most important control parameter to guide a winged
body through the flight corridor (see Fig. 10.22).
– Accordingly, the reentry of a Space Shuttle, which in this book even more
serves as a case study, is explained in Sect. 10.7 in greater detail and in terms of
NASA terminology.
– In Sect. 8.1, the different basic types of orbit maneuvers are discussed and
exemplified.
– A new form of solution of Lambert’s problem is derived in Sect. 8.2.3, which is
visualized in Fig. 8.8.
– Section 8.4.3 discusses modern super-synchronous transfer orbits to GEO.
– Relative motion in near-circular orbits is examined in Sect. 8.5.4.
– The virial theorem for bounded and unbounded n-body systems is derived in
Sect. 11.1.2 and used to discuss the stability of an n-body system.
– Section 12.3 (Gravitational Perturbation Effects) has been revised and greatly
extended including other and higher order perturbation terms.
– Chapter 14 has been radically revised: There is a new Sect. 14.1 on orbit
geometric issues (eclipse duration and access area) and a fully revised Sect. 14.2
on orbit determination. | en_US |