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| | TRAJECTORIES AND ORBITS |
 | | Before launching, the vehicle is at the Earth's distance from the Sun, moving with the Earth's speed around the sun-about 100,000 feet per second. |
 | | Starting from the surface of the Earth, a launch velocity of about 54,000 feet per second will lead to escape from the solar system The course of the vehicle will be a parabola, with the Sun at its focus; until eons later lt is deflected by some star or other body. |
 | | One kind of application of particular interest involves use of heavy conventional propulsion systems to develop orbital velocity (say, 25,000 feet per second) and then to build up the remaining 12,000 feet per second to reach escape velocity by a low-thrust electrical system. |
| www.hq.nasa.gov /office/pao/History/conghand/traject.htm (1856 words) |
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