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| Books | Books |
 III, the ion rocket engine has the potential capability of achieving larger values of specific impulse than any other type of rocket engine without introducing severe heat transfer problems. Its thrust-to-weight ratios are, however, the smallest. Although...  Panel on Science and Technology, Fourth Meeting: Hearings Before the ... - Page 35 by Panel on Science and Technology. Meeting - 1962 - 110 pages Full view -
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