TABLE S.1 Summary of Vision Missions (in Alphabetical Order) Evaluated by the Committee
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Vision Mission
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Cost Estimatea (billions)
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Technical Maturityb
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Worthy of Further Study as a Constellation Mission?
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Notes
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Advanced Compton Telescope (ACT)
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$1
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Medium
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No
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This mission does not benefit from Constellation.
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Generation-X (Gen-X)
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>$5
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Low
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Yes
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One Ares V launch of one 16-meter telescope is significantly simpler than the early proposed configurations.
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Cost estimates are weak. The additional mass capability could significantly reduce mirror development costs.
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Interstellar Probe
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$1-$5
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High—concept, instruments
Low—propulsion
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Yes
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Further study is needed of the benefits of additional launch mass enabled by Ares V, in particular alternative propulsion options.
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|
Kilometer-Baseline Far-Infrared/Submillimeter Interferometer
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>$5
|
Low
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No
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The need for Constellation is questionable, except for human servicing.
|
|
Modern Universe Space Telescope (MUST)
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>$5
|
High—mission concept, instruments
Low—assembly
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Yes
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Large one-piece, central mirror is possible with Ares V rather than a robotically assembled mirror.
|
|
Neptune Orbiter with Probes
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>$5
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High—mission concept, instruments
Low—propulsion and possibly lander
|
Yes
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Ares V could possibly obviate the need for aerocapture and/or nuclear-electric propulsion.
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|
Palmer Quest
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>$5
|
Low
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No
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This mission does not benefit from Constellation.
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Single Aperture Far Infrared Mission (SAFIR)
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>$5
|
Medium—mission concept
Low—cooling, detectors
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No
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This mission does not benefit from Constellation.
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Solar Polar Imager
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$1-$5
|
High—mission concept, instruments
Low—propulsion
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Yes
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Consider propulsion options enabled by Ares V.
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Stellar Imager
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$5
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Low
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Yes
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Could launch larger mirrors (2 meters vs. 1 meter) and a second hub on a single Ares V launch.
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Titan Explorer
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>$5
|
Low—requires aerocapture
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Yes
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Launch on Ares V may enable propulsive capture rather than aerocapture and shorten transit time.
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a Cost estimates based on data provided to the committee.
b Technical maturity based on data provided to the committee.
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