Structure and Composition of Pluto's Atmosphere from the New Horizons
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Chemical Composition of Pluto's Aerosols Analogues
EPSC Abstracts Vol. 13, EPSC-DPS2019-941-1, 2019 EPSC-DPS Joint Meeting 2019 c Author(s) 2019. CC Attribution 4.0 license. Chemical composition of Pluto’s aerosols analogues Lora Jovanovic (1), Thomas Gautier (1), Nathalie Carrasco (1), Véronique Vuitton (2), Cédric Wolters (2), François-Régis Orthous-Daunay (2), Ludovic Vettier (1), Laurène Flandinet (2) ([email protected]) (1) Laboratoire Atmosphères, Milieux, Observations Spatiales (LATMOS), Guyancourt, France (2) Institut de Planétologie et d’Astrophysique de Grenoble (IPAG), Grenoble, France Abstract Table 1: Types of Pluto’s aerosols analogues produced with the PAMPRE experiment. The discovery of haze in Pluto’s atmosphere on July 14th, 2015, has raised lots of questions. To help Corresponding understand the data provided by the New Horizons Composition of the gas mixture altitude on spacecraft, Pluto’s aerosols analogues were Pluto [2] synthetized and their chemical composition was 99% N2 : 1% CH4 : 500 ppm CO 400 km determined by high-resolution mass spectrometry 95% N2 : 5% CH4 : 500 ppm CO 600 km (Orbitrap technique). 2.2. High-resolution mass spectrometry 1. Introduction (HRMS) study On July 14th, 2015, when Pluto was flown by the New Horizons spacecraft, aerosols were detected in its We analyzed the soluble fraction of Pluto’s aerosols atmosphere, mainly composed of molecular nitrogen analogues, dissolved in a 50:50 (v/v)% methanol:acetonitrile mixture. The analytical N2, methane CH4, with around 500 ppm of carbon monoxide CO [1,2,3]. These aerosols aggregate into instrument used was the LTQ Orbitrap XL several thin haze layers that extend at more than (ThermoFisher Scientific). -
An Investigation of Aerogravity Assist at Titan and Triton for Capture Into Orbit About Saturn and Neptune 2Nd International Planetary Probe Workshop August 2004, USA
An Investigation of Aerogravity Assist at Titan and Triton for Capture into Orbit About Saturn and Neptune 2nd International Planetary Probe Workshop August 2004, USA Philip Ramsey(1) and James Evans Lyne(2) (1)Department of Mechanical, Aerospace and Biomedical Engineering The University of Tennessee Knoxville, TN 37996 USA [email protected] (2)Department of Mechanical, Aerospace and Biomedical Engineering The University of Tennessee Knoxville, TN 37996 USA [email protected] ABSTRACT proposed that an aerogravity assist maneuver at the moon Titan could be used to capture a probe Previous work by our group has shown that an into orbit about Saturn, using an aeroshell with a aerogravity assist maneuver at the moon Titan with a low to moderate lift-to-drag ratio (0.25 to could be used to capture a spacecraft into a 1.0).1 This approach provides for capture into closed orbit about Saturn if a nominal orbit about the gas giant, while avoiding the atmospheric profile at Titan is assumed. The very high entry speeds and aerothermal heating present study extends that work and examines environment inherent to a trajectory thru the the impact of atmospheric dispersions, variations atmosphere of Saturn itself. in the final target orbit and low density aerodynamics on the aerocapture maneuver. Titan is unique among moons in the solar Accounting for atmospheric dispersions system in that it has an atmosphere considerably substantially reduces the entry corridor width for thicker than Earth’s, with a ground level density a blunt configuration with a lift-to-drag ratio of of about 5.44 kg/m3. -
+ 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 -
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. -
What Is the Color of Pluto? - Universe Today
What is the Color of Pluto? - Universe Today space and astronomy news Universe Today Home Members Guide to Space Carnival Photos Videos Forum Contact Privacy Login NASA’s New Horizons spacecraft captured this high-resolution enhanced color view of http://www.universetoday.com/13866/color-of-pluto/[29-Mar-17 13:18:37] What is the Color of Pluto? - Universe Today Pluto on July 14, 2015. Credit: NASA/JHUAPL/SwRI WHAT IS THE COLOR OF PLUTO? Article Updated: 28 Mar , 2017 by Matt Williams When Pluto was first discovered by Clybe Tombaugh in 1930, astronomers believed that they had found the ninth and outermost planet of the Solar System. In the decades that followed, what little we were able to learn about this distant world was the product of surveys conducted using Earth-based telescopes. Throughout this period, astronomers believed that Pluto was a dirty brown color. In recent years, thanks to improved observations and the New Horizons mission, we have finally managed to obtain a clear picture of what Pluto looks like. In addition to information about its surface features, composition and tenuous atmosphere, much has been learned about Pluto’s appearance. Because of this, we now know that the one-time “ninth planet” of the Solar System is rich and varied in color. Composition: With a mean density of 1.87 g/cm3, Pluto’s composition is differentiated between an icy mantle and a rocky core. The surface is composed of more than 98% nitrogen ice, with traces of methane and carbon monoxide. Scientists also suspect that Pluto’s internal structure is differentiated, with the rocky material having settled into a dense core surrounded by a mantle of water ice. -
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. -
A New View of Haze Formation and Energy Balance in Triton's Cold And
EPSC Abstracts Vol. 13, EPSC-DPS2019-332-1, 2019 EPSC-DPS Joint Meeting 2019 c Author(s) 2019. CC Attribution 4.0 license. A New View of Haze Formation and Energy Balance in Triton’s Cold and Hazy Atmosphere Xi Zhang (1), Kazumasa Ohno (2), Darrell Strobel (3), Ryo Tazaki (4), and Satoshi Okuzumi (2) (1) University of California Santa Cruz, Santa Cruz, USA ([email protected]), (2) Tokyo Institute of Technology, Tokyo, Japan, (3) Johns Hopkins University, Baltimore, USA, (4) Tohoku University, Sendai, Japan Abstract missing coolant is needed to understand the energy balance in Triton’s lower atmosphere. This research on Neptune’s moon Triton consists of two parts. To start we built the first microphysical 2. Methods model of Triton haze formation including fractal aggregation of monomers and condensation of We have built the first bin-scheme microphysical supersaturated hydrocarbons and nitriles. Our model model for Triton’s haze and cloud formation. Our can explain the UV occultation and visible scattering model simulates the evolution of size distributions in observations from Voyager 2 spacecraft during the a one-dimensional framework with sedimentation, Neptune flyby. With our model we find that haze coagulation, condensation and vertical eddy mixing. particles play a dominant role in the energy balance We consider that the haze particles are initially in the lower atmosphere of Triton, which was composed of fractal aggregates—non-spherical neglected in previous studies. Future ice giant particles comprised of many many spherical missions with a Triton lander should be able to monomers—similar in previous studies on Titan and measure the infrared fluxes from the near-surface Pluto (e.g., Cabane et al. -
Neptune Polar Orbiter with Probes*
NEPTUNE POLAR ORBITER WITH PROBES* 2nd INTERNATIONAL PLANETARY PROBE WORKSHOP, AUGUST 2004, USA Bernard Bienstock(1), David Atkinson(2), Kevin Baines(3), Paul Mahaffy(4), Paul Steffes(5), Sushil Atreya(6), Alan Stern(7), Michael Wright(8), Harvey Willenberg(9), David Smith(10), Robert Frampton(11), Steve Sichi(12), Leora Peltz(13), James Masciarelli(14), Jeffrey Van Cleve(15) (1)Boeing Satellite Systems, MC W-S50-X382, P.O. Box 92919, Los Angeles, CA 90009-2919, [email protected] (2)University of Idaho, PO Box 441023, Moscow, ID 83844-1023, [email protected] (3)JPL, 4800 Oak Grove Blvd., Pasadena, CA 91109-8099, [email protected] (4)NASA Goddard Space Flight Center, Greenbelt, MD 20771, [email protected] (5)Georgia Institute of Technology, 320 Parian Run, Duluth, GA 30097-2417, [email protected] (6)University of Michigan, Space Research Building, 2455 Haward St., Ann Arbor, MI 48109-2143, [email protected] (7)Southwest Research Institute, Department of Space Studies, 1050 Walnut St., Suite 400, Boulder, CO 80302, [email protected] (8)NASA Ames Research Center, Moffett Field, CA 94035-1000, [email protected] (9)4723 Slalom Run SE, Owens Cross Roads, AL 35763, [email protected] (10) Boeing NASA Systems, MC H013-A318, 5301 Bolsa Ave., Huntington Beach, CA 92647-2099, [email protected] (11)Boeing NASA Systems, MC H012-C349, 5301 Bolsa Ave., Huntington Beach, CA 92647-2099 [email protected] (12)Boeing Satellite Systems, MC W-S50-X382, P.O. Box 92919, Los Angeles, CA 90009-2919, [email protected] (13) )Boeing NASA Systems, MC H013-C320, 5301 Bolsa Ave., Huntington Beach, CA 92647-2099, [email protected] (14)Ball Aerospace & Technologies Corp., P.O. -
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. -
Results from the New Horizons Encounter with Pluto
EPSC Abstracts Vol. 11, EPSC2017-140, 2017 European Planetary Science Congress 2017 EEuropeaPn PlanetarSy Science CCongress c Author(s) 2017 Results from the New Horizons encounter with Pluto C. B. Olkin (1), S. A. Stern (1), J. R. Spencer (1), H. A. Weaver (2), L. A. Young (1), K. Ennico (3) and the New Horizons Team (1) Southwest Research Institute, Colorado, USA, (2) Johns Hopkins University Applied Physics Laboratory, Maryland, USA (3) NASA Ames Research Center, California, USA ([email protected]) Abstract Hydra) and the various processes that would darken those surfaces over time [5]. In July 2015, the New Horizons spacecraft flew through the Pluto system providing high spatial resolution panchromatic and color visible light imaging, near-infrared composition mapping spectroscopy, UV airglow measurements, UV solar and radio uplink occultations for atmospheric sounding, and in situ plasma and dust measurements that have transformed our understanding of Pluto and its moons [1]. Results from the science investigations focusing on geology, surface composition and atmospheric studies of Pluto and its largest satellite Charon will be presented. We also describe the New Horizons extended mission. 1. Geology and Size Highlights from the geology investigation of Pluto Figure 1: The glacial ices of Sputnik Planitia. The include the discovery of a unexpected diversity of cellular pattern is a surface expression of mobile lid geomorpholgies across the surface, the discovery of a convection. The boundaries of the cells are troughs. deep basin (informally known as Sputnik Planitia) Despite it’s size of ~900,000 km2, there are no containing glacial ices undergoing mobile-lid identified craters across Sputnik Planitia. -
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. -
New Horizons SOC to Instrument Pipeline ICD
New Horizons SOC to Instrument Pipeline ICD September 2017 SwRI® Project 05310 Document No. 05310-SOCINST-01 Contract NASW-02008 Prepared by SOUTHWEST RESEARCH INSTITUTE® Space Science and Engineering Division 6220 Culebra Road, San Antonio, Texas 78228-0510 (210) 684-5111 FAX (210) 647-4325 Southwest Research Institute 05310-SOCINST-01 Rev 0 Chg 0 New Horizons SOC to Instrument Pipeline ICD Page ii New Horizons SOC to Instrument Pipeline ICD SwRI Project 05310 Document No. 05310-SOCINST-01 Contract NASW-02008 Prepared by: Joe Peterson 08 November 2013 Revised by: Brian Carcich August, 2014 Revised by: Tiffany Finley March, 2016 Revised by: Tiffany Finley October, 2016 Revised by: Brian Carcich December, 2016 Revised by: Tiffany Finley, Brian Carcich, PEPSSI team April, 2017 Revised by: Tiffany Finley, PEPSSI team September, 2017 Contributors: ALICE specifics prepared by: Maarten Versteeg, Joel Parker, & Andrew Steffl LEISA specifics prepared by: George McCabe & Allen Lunsford LORRI specifics prepared by: Hal Weaver & Howard Taylor MVIC specifics prepared by: Cathy Olkin PEPSSI specifics prepared by: Stefano Livi, Matthew Hill, Lawrence Brown, & Peter Kollman REX specifics prepared by: Ivan Linscott & Brian Carcich SDC specifics prepared by: David James SWAP specifics prepared by: Heather Elliott Southwest Research Institute 05310-SOCINST-01 Rev 0 Chg 0 New Horizons SOC to Instrument Pipeline ICD Page iii General Approval Signatures: Approved by: ____________________________________ Date: ____________ Hal Weaver, JHU/APL, Project Scientist