Combined Pluto Orbiter and Kuiper Belt Exploration Mission. C.J.A. Howett1, S
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Arxiv:2001.00125V1 [Astro-Ph.EP] 1 Jan 2020
Draft version January 3, 2020 Typeset using LATEX default style in AASTeX61 SIZE AND SHAPE CONSTRAINTS OF (486958) ARROKOTH FROM STELLAR OCCULTATIONS Marc W. Buie,1 Simon B. Porter,1 et al. 1Southwest Research Institute 1050 Walnut St., Suite 300, Boulder, CO 80302 USA To be submitted to Astronomical Journal, Version 1.1, 2019/12/30 ABSTRACT We present the results from four stellar occultations by (486958) Arrokoth, the flyby target of the New Horizons extended mission. Three of the four efforts led to positive detections of the body, and all constrained the presence of rings and other debris, finding none. Twenty-five mobile stations were deployed for 2017 June 3 and augmented by fixed telescopes. There were no positive detections from this effort. The event on 2017 July 10 was observed by SOFIA with one very short chord. Twenty-four deployed stations on 2017 July 17 resulted in five chords that clearly showed a complicated shape consistent with a contact binary with rough dimensions of 20 by 30 km for the overall outline. A visible albedo of 10% was derived from these data. Twenty-two systems were deployed for the fourth event on 2018 Aug 4 and resulted in two chords. The combination of the occultation data and the flyby results provides a significant refinement of the rotation period, now estimated to be 15.9380 ± 0.0005 hours. The occultation data also provided high-precision astrometric constraints on the position of the object that were crucial for supporting the navigation for the New Horizons flyby. This work demonstrates an effective method for obtaining detailed size and shape information and probing for rings and dust on distant Kuiper Belt objects as well as being an important source of positional data that can aid in spacecraft navigation that is particularly useful for small and distant bodies. -
Europa Clipper Mission
Europa Clipper Mission Send a highly capable, radiation-tolerant spacecraft in a long, looping orbit around Jupiter to perform repeated close flybys of the icy moon. This document has been reviewed and determined not to contain export controlled technical data. 1 Exploring Europa’s Habitability: ! Ingredients for Life" Mission Goal: Explore Europa to Investigate its Habitability e-, O+, S+, … Water: • Probable saltwater ocean, implied by surface geology and magnetic field radiation-produced oxidants: • Possible lakes within the ice shell, produced by local melting O2, H2O2, CH2O ~ 100 K Chemistry: • Ocean in direct contact with mantle rock, promoting chemical leaching • Dark red surface materials contain salts, probably from the ocean Energy: • Chemical energy might sustain life • Surface irradiation creates oxidants • Mantle rock-water reactions could create reductants (hydrothermal or serpentinization) ? Habitability Activity: • Geological activity “stirs the pot” hydrothermally produced reductants: H S, H , CH , Fe • Activity could be cyclical, as tied to Io 2 2 4 ? This document has been reviewed and determined not to contain export controlled technical data. 2 Workshop Overview" Project manager, Barry Goldstein, and Planetary Protection Officer, Lisa Pratt, collaborated on setting objectives for the three-day workshop: • Validate the modeling framework for Europa Clipper Planetary Protection. • Agree on model input values, or on a plan to derive/ identify appropriate model inputs. • Develop workshop concurrence regarding future research plans and their priority. Spoiler Alert The three objectives were accomplished. This document has been reviewed and determined not to contain export controlled technical data. 3 Outside Subject-Matter Experts" A panel of multidisciplinary experts were assembled to provide consultation and guidance at the workshop." This document has been reviewed and determined not to contain export controlled technical data. -
+ New Horizons
Media Contacts NASA Headquarters Policy/Program Management Dwayne Brown New Horizons Nuclear Safety (202) 358-1726 [email protected] The Johns Hopkins University Mission Management Applied Physics Laboratory Spacecraft Operations Michael Buckley (240) 228-7536 or (443) 778-7536 [email protected] Southwest Research Institute Principal Investigator Institution Maria Martinez (210) 522-3305 [email protected] NASA Kennedy Space Center Launch Operations George Diller (321) 867-2468 [email protected] Lockheed Martin Space Systems Launch Vehicle Julie Andrews (321) 853-1567 [email protected] International Launch Services Launch Vehicle Fran Slimmer (571) 633-7462 [email protected] NEW HORIZONS Table of Contents Media Services Information ................................................................................................ 2 Quick Facts .............................................................................................................................. 3 Pluto at a Glance ...................................................................................................................... 5 Why Pluto and the Kuiper Belt? The Science of New Horizons ............................... 7 NASA’s New Frontiers Program ........................................................................................14 The Spacecraft ........................................................................................................................15 Science Payload ...............................................................................................................16 -
Europa Clipper Mission: Preliminary Design Report
Europa Clipper Mission: Preliminary Design Report Todd Bayer, Molly Bittner, Brent Buffington, Karen Kirby, Nori Laslo Gregory Dubos, Eric Ferguson, Ian Harris, Johns Hopkins University Applied Physics Maddalena Jackson, Gene Lee, Kari Lewis, Jason Laboratory 11100 Johns Hopkins Road Laurel, Kastner, Ron Morillo, Ramiro Perez, Mana MD 20723-6099 Salami, Joel Signorelli, Oleg Sindiy, Brett Smith, [email protected] Melissa Soriano Jet Propulsion Laboratory California Institute of Technology 4800 Oak Grove Dr. Pasadena, CA 91109 818-354-4605 [email protected] Abstract—Europa, the fourth largest moon of Jupiter, is 1. INTRODUCTION believed to be one of the best places in the solar system to look for extant life beyond Earth. Exploring Europa to investigate its Europa’s subsurface ocean is a particularly intriguing target habitability is the goal of the Europa Clipper mission. for scientific exploration and the hunt for life beyond Earth. The 2011 Planetary Decadal Survey, Vision and Voyages, The Europa Clipper mission envisions sending a flight system, states: “Because of this ocean’s potential suitability for life, consisting of a spacecraft equipped with a payload of NASA- Europa is one of the most important targets in all of planetary selected scientific instruments, to execute numerous flybys of Europa while in Jupiter orbit. A key challenge is that the flight science” [1]. Investigation of Europa’s habitability is system must survive and operate in the intense Jovian radiation intimately tied to understanding the three “ingredients” for environment, which is especially harsh at Europa. life: liquid water, chemistry, and energy. The Europa Clipper mission would investigate these ingredients by The spacecraft is planned for launch no earlier than June 2023, comprehensively exploring Europa’s ice shell and liquid from Kennedy Space Center, Florida, USA, on a NASA supplied ocean interface, surface geology and surface composition to launch vehicle. -
1 the Atmosphere of Pluto As Observed by New Horizons G
The Atmosphere of Pluto as Observed by New Horizons G. Randall Gladstone,1,2* S. Alan Stern,3 Kimberly Ennico,4 Catherine B. Olkin,3 Harold A. Weaver,5 Leslie A. Young,3 Michael E. Summers,6 Darrell F. Strobel,7 David P. Hinson,8 Joshua A. Kammer,3 Alex H. Parker,3 Andrew J. Steffl,3 Ivan R. Linscott,9 Joel Wm. Parker,3 Andrew F. Cheng,5 David C. Slater,1† Maarten H. Versteeg,1 Thomas K. Greathouse,1 Kurt D. Retherford,1,2 Henry Throop,7 Nathaniel J. Cunningham,10 William W. Woods,9 Kelsi N. Singer,3 Constantine C. C. Tsang,3 Rebecca Schindhelm,3 Carey M. Lisse,5 Michael L. Wong,11 Yuk L. Yung,11 Xun Zhu,5 Werner Curdt,12 Panayotis Lavvas,13 Eliot F. Young,3 G. Leonard Tyler,9 and the New Horizons Science Team 1Southwest Research Institute, San Antonio, TX 78238, USA 2University of Texas at San Antonio, San Antonio, TX 78249, USA 3Southwest Research Institute, Boulder, CO 80302, USA 4National Aeronautics and Space Administration, Ames Research Center, Space Science Division, Moffett Field, CA 94035, USA 5The Johns Hopkins University Applied Physics Laboratory, Laurel, MD 20723, USA 6George Mason University, Fairfax, VA 22030, USA 7The Johns Hopkins University, Baltimore, MD 21218, USA 8Search for Extraterrestrial Intelligence Institute, Mountain View, CA 94043, USA 9Stanford University, Stanford, CA 94305, USA 10Nebraska Wesleyan University, Lincoln, NE 68504 11California Institute of Technology, Pasadena, CA 91125, USA 12Max-Planck-Institut für Sonnensystemforschung, 37191 Katlenburg-Lindau, Germany 13Groupe de Spectroscopie Moléculaire et Atmosphérique, Université Reims Champagne-Ardenne, 51687 Reims, France *To whom correspondence should be addressed. -
2018: Aiaa-Space-Report
AIAA TEAM SPACE TRANSPORTATION DESIGN COMPETITION TEAM PERSEPHONE Submitted By: Chelsea Dalton Ashley Miller Ryan Decker Sahil Pathan Layne Droppers Joshua Prentice Zach Harmon Andrew Townsend Nicholas Malone Nicholas Wijaya Iowa State University Department of Aerospace Engineering May 10, 2018 TEAM PERSEPHONE Page I Iowa State University: Persephone Design Team Chelsea Dalton Ryan Decker Layne Droppers Zachary Harmon Trajectory & Propulsion Communications & Power Team Lead Thermal Systems AIAA ID #908154 AIAA ID #906791 AIAA ID #532184 AIAA ID #921129 Nicholas Malone Ashley Miller Sahil Pathan Joshua Prentice Orbit Design Science Science Science AIAA ID #921128 AIAA ID #922108 AIAA ID #761247 AIAA ID #922104 Andrew Townsend Nicholas Wijaya Structures & CAD Trajectory & Propulsion AIAA ID #820259 AIAA ID #644893 TEAM PERSEPHONE Page II Contents 1 Introduction & Problem Background2 1.1 Motivation & Background......................................2 1.2 Mission Definition..........................................3 2 Mission Overview 5 2.1 Trade Study Tools..........................................5 2.2 Mission Architecture.........................................6 2.3 Planetary Protection.........................................6 3 Science 8 3.1 Observations of Interest.......................................8 3.2 Goals.................................................9 3.3 Instrumentation............................................ 10 3.3.1 Visible and Infrared Imaging|Ralph............................ 11 3.3.2 Radio Science Subsystem................................. -
DOE Could Improve Planning and Communication Related to Plutonium-238 And
United States Government Accountability Office Report to Congressional Requesters September 2017 SPACE EXPLORATION DOE Could Improve Planning and Communication Related to Plutonium- 238 and Radioisotope Power Systems Production Challenges Accessible Version GAO-17-673 September 2017 SPACE EXPLORATION DOE Could Improve Planning and Communication Related to Plutonium-238 and Radioisotope Power Systems Production Challenges Highlights of GAO-17-673, a report to congressional requesters Why GAO Did This Study What GAO Found NASA uses RPS to generate electrical The National Aeronautics and Space Administration (NASA) selects radioisotope power in missions in which solar power systems (RPS) for missions primarily based on the agency’s scientific panels or batteries would be objectives and mission destinations. Prior to the establishment of the Department ineffective. RPS convert heat of Energy’s (DOE) Supply Project in fiscal year 2011 to produce new plutonium- generated by the radioactive decay of 238 (Pu-238), NASA officials said that Pu-238 supply was a limiting factor in Pu-238 into electricity. DOE maintains selecting RPS-powered missions. After the initiation of the Supply Project, a capability to produce RPS for NASA however, NASA officials GAO interviewed said that missions are selected missions, as well as a limited and independently of decisions on how to power them. Once a mission is selected, aging supply of Pu-238 that will be NASA considers power sources early in its mission review process. Multiple depleted in the 2020s, according to NASA and DOE officials and factors could affect NASA’s demand for RPS and Pu-238. For example, high documentation. With NASA funding, costs associated with RPS and missions can affect the demand for RPS DOE initiated the Pu-238 Supply because, according to officials, NASA’s budget can only support one RPS Project in 2011, with a goal of mission about every 4 years. -
Abstracts of the 50Th DDA Meeting (Boulder, CO)
Abstracts of the 50th DDA Meeting (Boulder, CO) American Astronomical Society June, 2019 100 — Dynamics on Asteroids break-up event around a Lagrange point. 100.01 — Simulations of a Synthetic Eurybates 100.02 — High-Fidelity Testing of Binary Asteroid Collisional Family Formation with Applications to 1999 KW4 Timothy Holt1; David Nesvorny2; Jonathan Horner1; Alex B. Davis1; Daniel Scheeres1 Rachel King1; Brad Carter1; Leigh Brookshaw1 1 Aerospace Engineering Sciences, University of Colorado Boulder 1 Centre for Astrophysics, University of Southern Queensland (Boulder, Colorado, United States) (Longmont, Colorado, United States) 2 Southwest Research Institute (Boulder, Connecticut, United The commonly accepted formation process for asym- States) metric binary asteroids is the spin up and eventual fission of rubble pile asteroids as proposed by Walsh, Of the six recognized collisional families in the Jo- Richardson and Michel (Walsh et al., Nature 2008) vian Trojan swarms, the Eurybates family is the and Scheeres (Scheeres, Icarus 2007). In this theory largest, with over 200 recognized members. Located a rubble pile asteroid is spun up by YORP until it around the Jovian L4 Lagrange point, librations of reaches a critical spin rate and experiences a mass the members make this family an interesting study shedding event forming a close, low-eccentricity in orbital dynamics. The Jovian Trojans are thought satellite. Further work by Jacobson and Scheeres to have been captured during an early period of in- used a planar, two-ellipsoid model to analyze the stability in the Solar system. The parent body of the evolutionary pathways of such a formation event family, 3548 Eurybates is one of the targets for the from the moment the bodies initially fission (Jacob- LUCY spacecraft, and our work will provide a dy- son and Scheeres, Icarus 2011). -
1 the New Horizons Spacecraft Glen H. Fountain, David Y
The New Horizons Spacecraft Glen H. Fountain, David Y. Kusnierkiewicz, Christopher B. Hersman, Timothy S. Herder, Thomas B Coughlin, William T. Gibson, Deborah A. Clancy, Christopher C. DeBoy, T. Adrian Hill, James D. Kinnison, Douglas S. Mehoke, Geffrey K. Ottman, Gabe D. Rogers, S. Alan Stern, James M. Stratton, Steven R. Vernon, Stephen P. Williams Abstract The New Horizons spacecraft was launched on January 19, 2006. The spacecraft was designed to provide a platform for the seven instruments designated by the science team to collect and return data from Pluto in 2015 that would meet the requirements established by the National Aeronautics and Space Administration (NASA) Announcement of Opportunity AO-OSS-01. The design drew on heritage from previous missions developed at The Johns Hopkins University Applied Physics Laboratory (APL) and other NASA missions such as Ulysses. The trajectory design imposed constraints on mass and structural strength to meet the high launch acceleration consistent with meeting the AO requirement of returning data prior to the year 2020. The spacecraft subsystems were designed to meet tight resource allocations (mass and power) yet provide the necessary control and data handling finesse to support data collection and return when the one way light time during the Pluto fly-by is 4.5 hours. Missions to the outer regions of the solar system (where the solar irradiance is 1/1000 of the level near the Earth) require a Radioisotope Thermoelectric Generator (RTG) to supply electrical power. One RTG was available for use by New Horizons. To accommodate this constraint, the spacecraft electronics were designed to operate on less than 200 W. -
The Radioscience Experiment on New Horizons
The Radioscience Experiment on New Horizons Ivan R. Linscott(1), Michael K. Bird(2), David P. Hinson(1)(3), Martin Pätzold(2), and G. Lenard Tyler(1) (1)Stanford University,350 Serra Mall, Stanford, CA, 94305, [email protected] [email protected], [email protected], [email protected], [email protected] (2)Rhenish Institute for Environmental Research University of Cologne, Germany, (3)SETI Institute Abstract REX is the Radioscience Experiment in the payload on the New Horizons spacecraft en-route to its encounter with Pluto in July of 2015. REX will obtain the temperature and pressure profiles of Pluto's tenuous atmosphere while measuring radiometric temperature, gravitational moments and ionosphere structure. Additional targets of opportunity, at lower priority, include the search for an atmosphere at Charon, improved gravity precision and a bistatic surface scattering on Pluto. For all but radiometry, these measurements take advantage of a high-power, X- band uplink transmitted from the earth, received on the spacecraft with the aid of a high-gain antenna, a low-noise X-band receiver and an ultrastable oscillator (USO), as a frequency reference. This combination enables REX to sense Pluto's atmosphere with precision of ~ 0.1 Pa (1 μbar), and ~ 3 K, and a neutral number density of 4x1019/m3. Critical measurement techniques will be validated using results from the May 20, 2011, Lunar Occultation of New Horizons spacecraft. 1. Introduction New Horizons is a NSAS mission to Pluto launched on January 2006, with a nine year cruise and intended encounter with Pluto on July 14, 2015. -
Valuing Life Detection Missions Edwin S
Valuing life detection missions Edwin S. Kite* (University of Chicago), Eric Gaidos (University of Hawaii), Tullis C. Onstott (Princeton University). * [email protected] Recent discoveries imply that Early Mars was habitable for life-as-we-know-it (Grotzinger et al. 2014); that Enceladus might be habitable (Waite et al. 2017); and that many stars have Earth- sized exoplanets whose insolation favors surface liquid water (Dressing & Charbonneau 2013, Gaidos 2013). These exciting discoveries make it more likely that spacecraft now under construction – Mars 2020, ExoMars rover, JWST, Europa Clipper – will find habitable, or formerly habitable, environments. Did these environments see life? Given finite resources ($10bn/decade for the US1), how could we best test the hypothesis of a second origin of life? Here, we first state the case for and against flying life detection missions soon. Next, we assume that life detection missions will happen soon, and propose a framework (Fig. 1) for comparing the value of different life detection missions: Scientific value = (Reach × grasp × certainty × payoff) / $ (1) After discussing each term in this framework, we conclude that scientific value is maximized if life detection missions are flown as hypothesis tests. With hypothesis testing, even a nondetection is scientifically valuable. Should the US fly more life detection missions? Once a habitable environment has been found and characterized, life detection missions are a logical next step. Are we ready to do this? The case for emphasizing habitable environments, not life detection: Our one attempt to detect life, Viking, is viewed in hindsight as premature or at best uncertain. In-space life detection experiments are expensive. -
NASA Finds Neptune Moons Locked in 'Dance of Avoidance' 15 November 2019, by Gretchen Mccartney
NASA finds Neptune moons locked in 'dance of avoidance' 15 November 2019, by Gretchen McCartney Although the dance may appear odd, it keeps the orbits stable, researchers said. "We refer to this repeating pattern as a resonance," said Marina Brozovi?, an expert in solar system dynamics at NASA's Jet Propulsion Laboratory in Pasadena, California, and the lead author of the new paper, which was published Nov. 13 in Icarus. "There are many different types of 'dances' that planets, moons and asteroids can follow, but this one has never been seen before." Far from the pull of the Sun, the giant planets of the Neptune Moon Dance: This animation illustrates how the outer solar system are the dominant sources of odd orbits of Neptune's inner moons Naiad and gravity, and collectively, they boast dozens upon Thalassa enable them to avoid each other as they race dozens of moons. Some of those moons formed around the planet. Credit: NASA alongside their planets and never went anywhere; others were captured later, then locked into orbits dictated by their planets. Some orbit in the opposite direction their planets rotate; others swap orbits Even by the wild standards of the outer solar with each other as if to avoid collision. system, the strange orbits that carry Neptune's two innermost moons are unprecedented, according to Neptune has 14 confirmed moons. Neso, the newly published research. farthest-flung of them, orbits in a wildly elliptical loop that carries it nearly 46 million miles (74 million Orbital dynamics experts are calling it a "dance of kilometers) away from the planet and takes 27 avoidance" performed by the tiny moons Naiad years to complete.