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The envelope of ballistic trajectories and elliptic orbits
Author(s) -
Eugene I. Butikov
Publication year - 2015
Publication title -
american journal of physics
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.541
H-Index - 99
eISSN - 1943-2909
pISSN - 0002-9505
DOI - 10.1119/1.4928176
Subject(s) - physics , envelope (radar) , projectile , classical mechanics , celestial mechanics , gravitational field , kepler , gravitation , kepler problem , domain (mathematical analysis) , field (mathematics) , motion (physics) , elliptic orbit , boundary (topology) , simple (philosophy) , theoretical physics , aerospace engineering , mathematical analysis , stars , quantum mechanics , astronomy , radar , philosophy , mathematics , epistemology , pure mathematics , engineering
Simple geometric derivations are given for the shape of the “safety domain” boundary for the family of Keplerian orbits of equal energy in a central gravitational field and for projectile trajectories in a uniform field. Examples of practical uses of the envelope of the family of orbits are discussed and illustrated by computer simulations. This material is appropriate for physics teachers and undergraduate students studying classical mechanics and orbital motions.

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