A variety of plans were proposed, including using launch windows (not counting backups) for a Jupiter assist in 2014, 2026, 2038, and 2050 [{Category:Template redirects]]about every 12 years. The launch opportunity for the 2014 window passed, but for example it could have resulted in a Jupiter flyby by early 2016 and then go on to reach 200 AU by 2044. With an ion drive, a speed of about 7.9 AU/yr by the time its xenon propellant was depleted could be attained, enabling that 200 AU by 2044 and perhaps 1000 AU after one hundred years from launch. Different launch times and configurations have various timelines and options.
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| - Innovative Interstellar Explorer
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rdfs:comment
| - A variety of plans were proposed, including using launch windows (not counting backups) for a Jupiter assist in 2014, 2026, 2038, and 2050 [{Category:Template redirects]]about every 12 years. The launch opportunity for the 2014 window passed, but for example it could have resulted in a Jupiter flyby by early 2016 and then go on to reach 200 AU by 2044. With an ion drive, a speed of about 7.9 AU/yr by the time its xenon propellant was depleted could be attained, enabling that 200 AU by 2044 and perhaps 1000 AU after one hundred years from launch. Different launch times and configurations have various timelines and options.
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dbkwik:nasa/proper...iPageUsesTemplate
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abstract
| - A variety of plans were proposed, including using launch windows (not counting backups) for a Jupiter assist in 2014, 2026, 2038, and 2050 [{Category:Template redirects]]about every 12 years. The launch opportunity for the 2014 window passed, but for example it could have resulted in a Jupiter flyby by early 2016 and then go on to reach 200 AU by 2044. With an ion drive, a speed of about 7.9 AU/yr by the time its xenon propellant was depleted could be attained, enabling that 200 AU by 2044 and perhaps 1000 AU after one hundred years from launch. Different launch times and configurations have various timelines and options.
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