These formulae allow a fast and sufficiently accurate design of the rocket trajectory within the atmosphere; in the exo-atmospheric flight closed form solutions of the optimal problem of injection into orbit are provided. The second part of the book deals with re-entry trajectories.. The rocket's reentry trajectory is controlled by thrust and aerodynamic force; whereas the glide reusable vehicle is unpowered [44]. The glide vehicle generally has a high ratio of lift-to-drag configuration for enough aerodynamic performance [[45], [46]].

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Re-entry conditions for ICBM re-entry vehicles, depend on the velocity and flight-path angle of the booster at burnout. In either case, we must know how the re-entry trajectory affects a vehicle's maximum deceleration, heating, and accuracy, as well as the re-entry corridor's size.. Four Forces on a Rocket On this page: Four Forces in Flight External Factors Differences in the Application of the Forces The study of rockets is an excellent way for students to learn the basics of forces and the response of an object to external forces. The motion of an object in response to an external force was first accurately described over 300 years ago by Sir Isaac Newton, using his.

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