Vision and Voyages for Planetary Science in the - Solar System ...
Vision and Voyages for Planetary Science in the - Solar System ...
Vision and Voyages for Planetary Science in the - Solar System ...
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• Long-lived, flight qualified ASRGs, with lifetimes <strong>in</strong> excess of 15 years;<br />
• Lightweight materials <strong>for</strong> <strong>the</strong> orbiter structure <strong>and</strong> subsystems; <strong>and</strong><br />
• Thermal protection systems <strong>for</strong> <strong>the</strong> probe.<br />
Although <strong>the</strong> Uranus mission can be accomplished us<strong>in</strong>g chemical propulsion, <strong>the</strong> availability of<br />
a flight-tested, comparatively <strong>in</strong>expensive solar-electric propulsion module would result <strong>in</strong> both a wider<br />
range of launch dates <strong>and</strong> more mass <strong>in</strong> orbit around Uranus. Aerocapture capability would enhance a<br />
Uranus orbiter mission. For a Neptune orbiter, <strong>the</strong> advantages of aerocapture are enormous.<br />
Enceladus Orbiter<br />
The Enceladus Orbiter’s key scientific <strong>in</strong>struments are a mass spectrometer, a <strong>the</strong>rmal mapp<strong>in</strong>g<br />
radiometer, a dust analyzer, an imag<strong>in</strong>g camera, <strong>and</strong> a magnetometer. O<strong>the</strong>r than improvements <strong>in</strong> <strong>the</strong><br />
sensitivity <strong>and</strong> accuracy of <strong>the</strong> mass spectrometer <strong>and</strong> <strong>the</strong>rmal mapp<strong>in</strong>g radiometer <strong>in</strong> particular, which<br />
would enhance <strong>the</strong> scientific mission, <strong>the</strong> major technological challenge is ensur<strong>in</strong>g reliability <strong>and</strong><br />
lifetime of <strong>the</strong> ASRGs. The mission requires three ASRGs to deliver power throughout <strong>the</strong> Enceladus<br />
orbit phase, which lasts <strong>for</strong> at least a year beg<strong>in</strong>n<strong>in</strong>g 12 years after launch. Because of <strong>the</strong> potential<br />
habitability of Enceladus, planetary protection is an additional technological challenge <strong>for</strong> an orbiter<br />
mission.<br />
Venus Climate Mission<br />
The Venus Climate Mission (VCM) <strong>in</strong>cludes four dist<strong>in</strong>ct flight elements: <strong>the</strong> carrier spacecraft<br />
that becomes a Venus orbiter, a gondola/balloon system, a m<strong>in</strong>i-probe, <strong>and</strong> drop sondes. The packag<strong>in</strong>g<br />
of <strong>the</strong> m<strong>in</strong>i-probe <strong>and</strong> <strong>the</strong> drop sondes, especially <strong>in</strong>tegration of a sophisticated neutral mass spectrometer<br />
<strong>in</strong> <strong>the</strong> m<strong>in</strong>i-probe, is <strong>the</strong> key technological challenge of VCM. Although each of <strong>the</strong> components of <strong>the</strong><br />
entry flight system, which conta<strong>in</strong>s <strong>the</strong> gondola <strong>and</strong> <strong>the</strong> balloon, is close to TRL 6, <strong>in</strong>dicat<strong>in</strong>g<br />
technological maturity, <strong>the</strong> entry flight system itself is still a significant design <strong>and</strong> development<br />
challenge. The management of <strong>the</strong> power, mass, <strong>and</strong> volume of this “Russian doll” vehicle throughout its<br />
design cycle could be viewed as a technology development <strong>in</strong> its own right.<br />
Future Mission Capabilities: 2023-2032<br />
Dur<strong>in</strong>g <strong>the</strong> com<strong>in</strong>g decade, <strong>the</strong> missions recommended by this decadal survey will address <strong>the</strong><br />
most compell<strong>in</strong>g science objectives with<strong>in</strong> <strong>the</strong> limited resources available to NASA. It is essential that<br />
<strong>the</strong> <strong>Planetary</strong> <strong>Science</strong> Division also <strong>in</strong>vest <strong>in</strong> <strong>the</strong> technological capabilities that will enable missions <strong>in</strong> <strong>the</strong><br />
follow<strong>in</strong>g decade. Dur<strong>in</strong>g <strong>the</strong> course of this decadal survey, a number of mission concepts have been<br />
studied to assess <strong>the</strong>ir cost, feasibility, <strong>and</strong> scientific value, <strong>and</strong> <strong>the</strong>se studies provide <strong>the</strong> foundation <strong>for</strong><br />
important technology <strong>in</strong>vestments. Table 11.1 summarizes <strong>the</strong>se missions <strong>and</strong> <strong>the</strong>ir key technology<br />
drivers. The committee strongly recommends that NASA strive to achieve balance <strong>in</strong> its technology<br />
<strong>in</strong>vestment programs by address<strong>in</strong>g both <strong>the</strong> near-term missions cited specifically <strong>in</strong> this report, as<br />
well as <strong>the</strong> longer-term missions that will be studied <strong>and</strong> prioritized <strong>in</strong> <strong>the</strong> future.<br />
PREPUBLICATION COPY—SUBJECT TO FURTHER EDITORIAL CORRECTION<br />
11-8