Previous article | Next article | This volume | Table of contents | Article options & Content finder |
Eur. J. Phys. 24 (March 2003) 175-183
Received 11 October 2002
Published 10 February
2003
Abstract. Various properties of Keplerian orbits traced by satellites that are launched from one and the same spatial point with different initial velocities are discussed. Two families of elliptical orbits are investigated, namely the sets of orbits produced by a common direction but different magnitudes of the initial velocities, and by a common magnitude but various directions of the initial velocities. For the latter family, the envelope of all the orbits is found, which is the boundary of the spatial region occupied by the orbits.
URL: stacks.iop.org/0143-0807/24/175 |
|
Previous article | Next article | This volume | Table of contents | |||||
| |||||
Setup information is available for Adobe
Acrobat. EndNote, ProCite ® and Reference Manager ® are registered trademarks of ISI Researchsoft. Copyright © Institute of Physics and IOP Publishing Limited 2003. Use of this service is subject to compliance with the terms and conditions of use. Systematic downloading of files is prohibited. |