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A Small Satellite Concept to Probe the Atmospheres of Uranus and Neptune Using Stellar Occultations
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Recent Mid-Infrared Through Submillimeter Observations of Uranus and Neptune
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Interiors of the Midsized Moons of Uranus, Degree-Two Gravity Fields, and Electromagnetic Properties from Coupled Physical and Chemical Modeling
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Thermal Protection Design for Uranus Orbiter Flagship Mission: Probes and Aerocapture
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Design Implications for Aerocapture Systems Placing Flagship-Class Uranus Orbiters
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Lessons From Pluto for Uranus Moons
Introduction: Small patches of starkly different albedo on both Oberon and Umbriel may be evidence for frost segregation and volatile migration. The high obliquity of the Uranian system makes it a good candidate for volatile transport activity. CO 2 and ammonium species have been detected on some Uranian satellites, and CH 4 is at least theoretically viable as a resident volatile. The OWL-recommended UOP Orbiter spacecraft should be equipped with instruments capable of evaluating the nature and extent of volatiles in the Uranian satellite system.
Shadow Chaser: A Small Satellite Concept to Probe the Atmospheres of Uranus and Neptune Using Stellar Occultations
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6-DOF Uranus Aerocapture Trajectory Analysis
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Uranus Orbiter Probe Drivers and Trades
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The Uranus Flagship: Investigating New Paradigms for Outer Solar System Exploration Workshop Summary Report
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Aerocapture as an Enabling Technology for Uranus Flagship Mission
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TPS Technology Status on Enabling New Frontiers Sample Return Missions from Moon, Asteroids and Comets and Probe Missions to Saturn and Uranus
STMD and SMD investment in TPS technology development such as Heatshield for Extreme Entry Environment (HEEET), 3-D woven Mid-Density Carbon Phenolic (3MDCP) and Conformal PICA over the past decade in response the the Decadal Committee Recommendation (2012). 3MDCP, a variant of HEEET, is baselined as the TPS for MSR, HEEET is enabling the Rocket Lab mission to Venus and Conformal PICA enabled VARDA as the heat shield TPS for their sample return capsule Winnebago-1. In the meantime, PICA, the TPS that enabled Stardust and OSIRIS-REx has atrophied. While these are success stories, upcoming NF-5/6 AO is anticipated to have multiple proposals that may be more demanding for sample return missions from Moon, Asteroids and Comets, and in addition probe missions to Saturn and UOP . This poster will address the state-of-the-art TPS for NF-5/6 in-situ and sample return missions, and for the UOP flagship mission. The poster will focus on steps that need to be taken to both advance and sustain NASA developed TPS and be ready to enable NF-5/6 and Flagship missions.
Compositions and Interior Structures of the Large Moons of Uranus and Implications for Future Spacecraft Observations
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Ring Seismology of the Ice Giants Uranus and Neptune
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Auroral and Non‐Auroral H 3 + Ion Winds at Uranus With Keck‐NIRSPEC and IRTF‐iSHELL
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