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	<title>Innovative Interstellar Explorer - Revision history</title>
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		<title>imported&gt;TheFugeni: /* top */Fixed typo</title>
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		<updated>2024-10-05T14:54:17Z</updated>

		<summary type="html">&lt;p&gt;&lt;span class=&quot;autocomment&quot;&gt;top: &lt;/span&gt;Fixed typo&lt;/p&gt;
&lt;p&gt;&lt;b&gt;New page&lt;/b&gt;&lt;/p&gt;&lt;div&gt;{{short description|NASA proposed space probe to 1000 AU from the Sun}}&lt;br /&gt;
[[File:Innovative Interstellar Explorer interstellar space probe .jpg|thumb|Early concept art for the explorer]]&lt;br /&gt;
&amp;#039;&amp;#039;&amp;#039;Innovative Interstellar Explorer&amp;#039;&amp;#039;&amp;#039; was a [[NASA]] &amp;quot;Vision Mission&amp;quot; study funded by NASA following a proposal under NRA-03-OSS-01 on 11&amp;amp;nbsp;September 2003. This study focused on measuring the [[interstellar medium]], the region outside the influence of the nearest star, the [[Sun]].&amp;lt;ref name=NASA&amp;gt;{{cite web|url=http://interstellarexplorer.jhuapl.edu/mission/implementation.html |title=Innovative Interstellar Probe|author=NASA}}&amp;lt;/ref&amp;gt; It proposes to use a [[radioisotope thermal generator]] to power [[ion thruster]]s.&amp;lt;ref name=NASA/&amp;gt; &lt;br /&gt;
&lt;br /&gt;
The project is a study of a proposed interstellar precursor mission that would probe the nearby interstellar medium and measure the properties of magnetic fields and [[cosmic ray]]s and their effects on a spacecraft leaving the [[Solar System]].&amp;lt;ref name=David /&amp;gt; Mission launch plans analyzed direct, one planet, multi-planet, and upper-stage trades.&amp;lt;ref name=NASA2&amp;gt;{{cite web|url=http://interstellarexplorer.jhuapl.edu/mission/mission_design_req.html |title=Innovative Interstellar Probe: Mission Design Requirements|author=NASA}}&amp;lt;/ref&amp;gt; As a concept study, a number of technologies, configurations, and mission goals were considered, leading to the choice of a spacecraft propelled with [[ion engine]]s powered by a [[radioisotope thermoelectric generator]] (RTG).&amp;lt;ref name=&amp;quot;esa.int&amp;quot;&amp;gt;[http://www.esa.int/gsp/ACT/doc/MAD/ACT-PRE-MAD-InnSys-McNutt.pdf &amp;#039;&amp;#039;Innovative Interstellar Explorer&amp;#039;&amp;#039; Feb 2006] slides&amp;lt;/ref&amp;gt; The focus was getting a spacecraft launched by about 2014, achieving 200 AU by the year 2031.&amp;lt;ref&amp;gt;[http://authors.library.caltech.edu/6296/1/MCNaipcp06.pdf &amp;#039;&amp;#039;Innovative interstellar explorer&amp;#039;&amp;#039;] 7 pages&amp;lt;/ref&amp;gt;&lt;br /&gt;
&lt;br /&gt;
A variety of strategies were assessed, including using launch windows (not counting backups) for a Jupiter assist in 2014, 2026, 2038, and 2050{{mdash}}about every 12 years.&amp;lt;ref name=NASA2/&amp;gt; &lt;br /&gt;
The launch opportunity for the 2014 window passed,&amp;lt;ref&amp;gt;{{cite web|url=http://www.centauri-dreams.org/?p=21050|title=Update on Innovative Interstellar Explorer |first=Paul |last=Gilster |date=December 20, 2011}}&amp;lt;/ref&amp;gt; but for example it could have resulted in a Jupiter flyby by early 2016 and then go on to reach 200 [[astronomical units]] (AU) by 2044.&amp;lt;ref name=NASA2/&amp;gt;&amp;lt;ref name=David&amp;gt;{{cite web |url=http://www.space.com/businesstechnology/050706_star_voyage.html |title=Voyage to the Stars: NASA Study Mulls Options  |work=[[Space.com]] |author=David, Leonard |date=July 6, 2005}}&amp;lt;/ref&amp;gt; With an ion drive, a speed of about 7.9&amp;amp;nbsp;AU per year could be attained by the time its [[xenon]] propellant was depleted, enabling a travel distance of 200&amp;amp;nbsp;AU by 2044 and perhaps 1000&amp;amp;nbsp;AU after one hundred years from launch.&amp;lt;ref name=NASA2/&amp;gt; Different launch times and configurations have various timelines and options.&amp;lt;ref name=NASA2/&amp;gt; One configuration for launch saw the use of a [[Delta IV Heavy]] and for the upper stages a stack of [[Star 48]] and [[Star 37]] leading to various gravity assist options.&amp;lt;ref name=&amp;quot;esa.int&amp;quot;/&amp;gt; Another launch stack that was considered was the [[Atlas V 551]] with a Star 48.&amp;lt;ref name=&amp;quot;esa.int&amp;quot;/&amp;gt;&lt;br /&gt;
&lt;br /&gt;
In 2011, the study&amp;#039;s primary author gave an update to website [[Centauri Dreams]], giving a retrospective on the mission and its feasibility since its publication in 2003.&amp;lt;ref name=&amp;quot;centauri-dreams.org&amp;quot;&amp;gt;{{Cite news|url=http://www.centauri-dreams.org/?p=21050|title=Update on Innovative Interstellar Explorer|date=2011-12-20|newspaper=Centauri Dreams|access-date=2017-02-21|language=en-US}}&amp;lt;/ref&amp;gt; By that time, some of the earliest launch windows were no longer feasible without a ready spacecraft.&amp;lt;ref name=&amp;quot;centauri-dreams.org&amp;quot;/&amp;gt; Some retrospectives were the advantages and potential of [[solar sail]]s, but the need for them to be more advanced for a mission, and also the utility of a radioisotope propulsion (REP) for such a mission.&amp;lt;ref name=&amp;quot;centauri-dreams.org&amp;quot;/&amp;gt; REP was the combination of using an RTG to power an ion drive.&amp;lt;ref name=&amp;quot;centauri-dreams.org&amp;quot;/&amp;gt;&lt;br /&gt;
&lt;br /&gt;
==See also==&lt;br /&gt;
*[[Applied Physics Laboratory]]&lt;br /&gt;
*[[Interstellar probe]]&lt;br /&gt;
*[[New Horizons 2]]&lt;br /&gt;
*[[New Horizons]] (Pluto flyby 2015, now heading out to KBOs)&lt;br /&gt;
*[[TAU (spacecraft)]]&lt;br /&gt;
&lt;br /&gt;
== References ==&lt;br /&gt;
{{reflist}}&lt;br /&gt;
&lt;br /&gt;
==External links==&lt;br /&gt;
*[http://interstellarexplorer.jhuapl.edu/index.php Interstellar Explorer – NASA]&lt;br /&gt;
*[http://www.esa.int/gsp/ACT/doc/MAD/ACT-PRE-MAD-InnSys-McNutt.pdf Presentation on IIE]&lt;br /&gt;
&lt;br /&gt;
{{Jupiter spacecraft}}&lt;br /&gt;
&lt;br /&gt;
[[Category:Hypothetical spacecraft]]&lt;br /&gt;
[[Category:Interstellar travel]]&lt;br /&gt;
[[Category:Proposed space probes]]&lt;/div&gt;</summary>
		<author><name>imported&gt;TheFugeni</name></author>
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