Shoot the Moon
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Selection of the Insight Landing Site M. Golombek1, D. Kipp1, N
Manuscript Click here to download Manuscript InSight Landing Site Paper v9 Rev.docx Click here to view linked References Selection of the InSight Landing Site M. Golombek1, D. Kipp1, N. Warner1,2, I. J. Daubar1, R. Fergason3, R. Kirk3, R. Beyer4, A. Huertas1, S. Piqueux1, N. E. Putzig5, B. A. Campbell6, G. A. Morgan6, C. Charalambous7, W. T. Pike7, K. Gwinner8, F. Calef1, D. Kass1, M. Mischna1, J. Ashley1, C. Bloom1,9, N. Wigton1,10, T. Hare3, C. Schwartz1, H. Gengl1, L. Redmond1,11, M. Trautman1,12, J. Sweeney2, C. Grima11, I. B. Smith5, E. Sklyanskiy1, M. Lisano1, J. Benardino1, S. Smrekar1, P. Lognonné13, W. B. Banerdt1 1Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109 2State University of New York at Geneseo, Department of Geological Sciences, 1 College Circle, Geneseo, NY 14454 3Astrogeology Science Center, U.S. Geological Survey, 2255 N. Gemini Dr., Flagstaff, AZ 86001 4Sagan Center at the SETI Institute and NASA Ames Research Center, Moffett Field, CA 94035 5Southwest Research Institute, Boulder, CO 80302; Now at Planetary Science Institute, Lakewood, CO 80401 6Smithsonian Institution, NASM CEPS, 6th at Independence SW, Washington, DC, 20560 7Department of Electrical and Electronic Engineering, Imperial College, South Kensington Campus, London 8German Aerospace Center (DLR), Institute of Planetary Research, 12489 Berlin, Germany 9Occidental College, Los Angeles, CA; Now at Central Washington University, Ellensburg, WA 98926 10Department of Earth and Planetary Sciences, University of Tennessee, Knoxville, TN 37996 11Institute for Geophysics, University of Texas, Austin, TX 78712 12MS GIS Program, University of Redlands, 1200 E. Colton Ave., Redlands, CA 92373-0999 13Institut Physique du Globe de Paris, Paris Cité, Université Paris Sorbonne, France Diderot Submitted to Space Science Reviews, Special InSight Issue v. -
Prescriptions for Excellence in Health Care a Collaboration Between Jefferson School of Population Health and Lilly Usa, Llc
PRESCRIPTIONS FOR EXCELLENCE IN HEALTH CARE A COLLABORATION BETWEEN JEFFERSON SCHOOL OF POPULATION HEALTH AND LILLY USA, LLC ISSUE 23 | WINTER 2015 EDITORIAL TABLE OF CONTENTS ACOs Due for Their Annual Checkup David B. Nash, MD, MBA A Message from Lilly: Opportunities, Uncertainty Loom in 2015 for the Editor-in-Chief Health Exchange Marketplace Ryan Urgo, MPP ....................................................2 As 2013 drew to a close, Premier with more than 190,000 physicians Healthcare Alliance predicted and other health care professionals Biography of a New ACO Joel Port, FACHE .............................................4 that participation in accountable participating.2 Although the care organizations (ACOs) would number of Medicare ACOs has Evolving Health Care Models and double in 2014 as a result of more grown more rapidly than the the Impact on Value and Quality providers developing core ACO number of non-Medicare ACOs, Bruce Perkins ...................................................6 capabilities.1 Premier’s forecast 46-52 million Americans (15%- Employers and Accountable Care was made on the basis of its 18% of the total population) are Organizations: A Good Marriage? survey of 115 senior executives patients in organizations with ACO Laurel Pickering, MPH .....................................9 that revealed a growing trend in arrangements with at least 1 payer.2 high-risk population management, coupled with reductions in cost The next question is, are ACOs and increases in health care quality doing what they are designed to do and patient satisfaction. Of those (ie, improving quality and lowering who responded: costs)? Although it is far too early to draw conclusions, the Centers • More than 75% reported for Medicare & Medicaid Services Prescriptions for Excellence in Health that they were integrating (CMS) has begun to release Care is brought to Population Health clinical and claims data to financial and quality outcomes. -
Rideshare and the Orbital Maneuvering Vehicle: the Key to Low-Cost Lagrange-Point Missions
SSC15-II-5 Rideshare and the Orbital Maneuvering Vehicle: the Key to Low-cost Lagrange-point Missions Chris Pearson, Marissa Stender, Christopher Loghry, Joe Maly, Valentin Ivanitski Moog Integrated Systems 1113 Washington Avenue, Suite 300, Golden, CO, 80401; 303 216 9777, extension 204 [email protected] Mina Cappuccio, Darin Foreman, Ken Galal, David Mauro NASA Ames Research Center PO Box 1000, M/S 213-4, Moffett Field, CA 94035-1000; 650 604 1313 [email protected] Keats Wilkie, Paul Speth, Trevor Jackson, Will Scott NASA Langley Research Center 4 West Taylor Street, Mail Stop 230, Hampton, VA, 23681; 757 864 420 [email protected] ABSTRACT Rideshare is a well proven approach, in both LEO and GEO, enabling low-cost space access through splitting of launch charges between multiple passengers. Demand exists from users to operate payloads at Lagrange points, but a lack of regular rides results in a deficiency in rideshare opportunities. As a result, such mission architectures currently rely on a costly dedicated launch. NASA and Moog have jointly studied the technical feasibility, risk and cost of using an Orbital Maneuvering Vehicle (OMV) to offer Lagrange point rideshare opportunities. This OMV would be launched as a secondary passenger on a commercial rocket into Geostationary Transfer Orbit (GTO) and utilize the Moog ESPA secondary launch adapter. The OMV is effectively a free flying spacecraft comprising a full suite of avionics and a propulsion system capable of performing GTO to Lagrange point transfer via a weak stability boundary orbit. In addition to traditional OMV ’tug’ functionality, scenarios using the OMV to host payloads for operation at the Lagrange points have also been analyzed. -
Space Isotopic Power Systems
Space isotopiC power systems With the technology sound and growing, and units already built for missions ranging from 120 days to 5 years, the designer can and should plan appropriate space application of isotopic systems BY CAPT. R. T. CARPENTER, USAF U.S. Atomic Energy Commission A new space power system technology technology, and aerospace nuclear Concurrently, the terrestrial appli -isotopic power-has developed to safety technology contributed by the cations-the Snap-7 programs-sus the point where it can and should be program and used as a foundation for tained the isotopic power development considered by the space-vehicle de follow-on space isotopic power-system program and promoted the fission signer for use in many types of mis developments. product separations and processing sions. Because of this sound technical capability that exists within the Com The' Atomic Energy Commission's basis, the Commission's space-oriented mission today! The interest among isotopic space power program dates isotopic power development program terrestrial power users-the Navy, back to several years before Sputnik has made a steady, although some Weather Bureau, and Coast Guard I, but the program suffered a severe times slow, comeback through a series was sufficiently strong to sup:port this setback in 1959 when the Snap-1A of events since 1959, so that today a . fuels production program, whe:r:eas the generator development program was program technically comparable to interest in Snap-1A had been inade cancelled.' This pioneer program was Snap-1A could once more be under quate. At the same time, significant not completed because it may have taken with a high probability of suc quantities of the long-lived alpha been tt;lO ambitious for its day. -
Indication, from Pioneer 10/11, Galileo and Ulysses Data, of an Apparent Anomalous, Weak, Long-Range Acceleration”
View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by CERN Document Server Comment on \Indication, from Pioneer 10/11, Galileo and Ulysses Data, of an Apparent Anomalous, Weak, Long-Range Acceleration" J. I. Katz Department of Physics and McDonnell Center for the Space Sciences Washington U., St. Louis, Mo. 63130 [email protected] (December 4, 1998) Pacs numbers: 04.80.-y, 95.10.Eg, 95.55.Pe Typeset using REVTEX 1 This paper [1] may have underestimated the acceleration resulting from the radiation of waste heat by the Pioneer spacecraft RTG. These generators are not very efficient; theoretical efficiencies may be as high as 20% [2] but RTG used in spacecraft more typically have electrical efficiencies of about 6% when new [3], which decline slowly as the thermoelectric material degrades and radioactive decay reduces the Carnot efficiency. Specific parameters and detailed design information for Pioneer are difficult to obtain so I adopt an initial electrical efficiency of 6%. Then the electric power at launch of 160 W [1] implied a thermal power of 2.67 kW and a waste heat of 2.51 kW. In 1997 the thermal power, decaying with thehalflifeofPu238 of 87.74 y, was 2.19 kW and the electrical power of 80 W [1] implied a waste heat of 2.11 kW. The power of a collimated beam sufficient to explain the reported anomalous acceleration aP is 85 W [1]. The same force can be obtained from the present rejected waste heat if it is radiated with cos θ =0:040, where θ is the angle between the direction of radiation and a ray from the Sun.h Ifi the 72 W of dissipated electrical power (allowing for 8 W radiated by the antenna) are radiated from the back of the spacecraft according to Lambert’s law the RTG waste heat need only give the thrust of a 37 W collimated beam, requiring cos θ =0:018. -
Water on the Moon, III. Volatiles & Activity
Water on The Moon, III. Volatiles & Activity Arlin Crotts (Columbia University) For centuries some scientists have argued that there is activity on the Moon (or water, as recounted in Parts I & II), while others have thought the Moon is simply a dead, inactive world. [1] The question comes in several forms: is there a detectable atmosphere? Does the surface of the Moon change? What causes interior seismic activity? From a more modern viewpoint, we now know that as much carbon monoxide as water was excavated during the LCROSS impact, as detailed in Part I, and a comparable amount of other volatiles were found. At one time the Moon outgassed prodigious amounts of water and hydrogen in volcanic fire fountains, but released similar amounts of volatile sulfur (or SO2), and presumably large amounts of carbon dioxide or monoxide, if theory is to be believed. So water on the Moon is associated with other gases. Astronomers have agreed for centuries that there is no firm evidence for “weather” on the Moon visible from Earth, and little evidence of thick atmosphere. [2] How would one detect the Moon’s atmosphere from Earth? An obvious means is atmospheric refraction. As you watch the Sun set, its image is displaced by Earth’s atmospheric refraction at the horizon from the position it would have if there were no atmosphere, by roughly 0.6 degree (a bit more than the Sun’s angular diameter). On the Moon, any atmosphere would cause an analogous effect for a star passing behind the Moon during an occultation (multiplied by two since the light travels both into and out of the lunar atmosphere). -
NASA and Planetary Exploration
**EU5 Chap 2(263-300) 2/20/03 1:16 PM Page 263 Chapter Two NASA and Planetary Exploration by Amy Paige Snyder Prelude to NASA’s Planetary Exploration Program Four and a half billion years ago, a rotating cloud of gaseous and dusty material on the fringes of the Milky Way galaxy flattened into a disk, forming a star from the inner- most matter. Collisions among dust particles orbiting the newly-formed star, which humans call the Sun, formed kilometer-sized bodies called planetesimals which in turn aggregated to form the present-day planets.1 On the third planet from the Sun, several billions of years of evolution gave rise to a species of living beings equipped with the intel- lectual capacity to speculate about the nature of the heavens above them. Long before the era of interplanetary travel using robotic spacecraft, Greeks observing the night skies with their eyes alone noticed that five objects above failed to move with the other pinpoints of light, and thus named them planets, for “wan- derers.”2 For the next six thousand years, humans living in regions of the Mediterranean and Europe strove to make sense of the physical characteristics of the enigmatic planets.3 Building on the work of the Babylonians, Chaldeans, and Hellenistic Greeks who had developed mathematical methods to predict planetary motion, Claudius Ptolemy of Alexandria put forth a theory in the second century A.D. that the planets moved in small circles, or epicycles, around a larger circle centered on Earth.4 Only partially explaining the planets’ motions, this theory dominated until Nicolaus Copernicus of present-day Poland became dissatisfied with the inadequacies of epicycle theory in the mid-sixteenth century; a more logical explanation of the observed motions, he found, was to consider the Sun the pivot of planetary orbits.5 1. -
Lessons from the Pioneer Venus Program
https://ntrs.nasa.gov/search.jsp?R=20070014676 2019-08-29T18:39:07+00:00Z View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by NASA Technical Reports Server LESSONS FROM THE PIONEER VENUS PROGRAM Steven D. Dorfman Boeing Satellite Systems, P.O. Box 92919, Los Angeles, CA 90009-2919 Good evening. It is indeed a pleasure to address a than my six years heading up the Pioneer Venus pro- group of scientists and engineers who share my enthu- gram for Hughes. siasm for space exploration. When Bernie Bienstock, tonight’s host from Boeing, first asked me to be a key- My planetary exploration experience began in the early note speaker tonight he suggested I tell war stories 70’s with the Outer Planets Grand Tour. At that time, about Pioneer Venus. Well, for a veteran like me, that’s the alignment of the outer planets presented a unique a tempting offer. And it’s a temptation I don’t intend to opportunity to fly a single spacecraft to Jupiter, Saturn, resist. So my remarks tonight will be more of a per- Uranus, Neptune and Pluto. In fact, this opportunity sonal Pioneer Venus memoir then a program history. was singled out by President Nixon as a major national As the Hughes Program Manager for the Pioneer Ve- objective, in much the same way President Bush has nus project, I gained a perspective on what it takes to announced the missions to the Moon, Mars and beyond design, build, test, launch and fly planetary missions. -
Proposal Information Package
NASA RESEARCH ANNOUNCEMENT PROPOSAL INFORMATION PACKAGE Mars Exploration Program 2001 Mars Odyssey Orbiter 23 July 2001 Contributors Raymond Arvidson1 Jeffrey J. Plaut5 Gautam Badhwar2 Susan Slavney1 William Boynton3 David A. Spencer5 Philip Christensen4 Compiled by Thomas W. Thompson5 Jeffrey J. Plaut5 Catherine M. Weitz6 1Washington University, 2Johnson Space Center, 3Lunar and Planetary Laboratory (University of Arizona), 4Arizona State University, 5Jet Propulsion Laboratory, California Institute of Technology 6NASA Headquarters. Table of Contents 1.0 Overview..............................................................................................................................................................1-1 1.1 Document Overview.............................................................................................................................1-1 1.2 Mars Exploration Program...................................................................................................................1-1 1.3 Mars 2001 Objectives...........................................................................................................................1-2 1.4 Mars 2001 Operations Management....................................................................................................1-2 1.5 Mars 2001 Orbiter Measurement Synergies through Coordinated Operations Planning ..................1-2 1.6 Mars 2001 Project Science Group (PSG) Members............................................................................1-3 2.0 Mars -
Locations of Anthropogenic Sites on the Moon R
Locations of Anthropogenic Sites on the Moon R. V. Wagner1, M. S. Robinson1, E. J. Speyerer1, and J. B. Plescia2 1Lunar Reconnaissance Orbiter Camera, School of Earth and Space Exploration, Arizona State University, Tempe, AZ 85287-3603; [email protected] 2The Johns Hopkins University, Applied Physics Laboratory, Laurel, MD 20723 Abstract #2259 Introduction Methods and Accuracy Lunar Reconnaissance Orbiter Camera (LROC) Narrow Angle Camera To get the location of each object, we recorded its line and sample in (NAC) images, with resolutions from 0.25-1.5 m/pixel, allow the each image it appears in, and then used USGS ISIS routines to extract identifcation of historical and present-day landers and spacecraft impact latitude and longitude for each point. The true position is calculated to be sites. Repeat observations, along with recent improvements to the the average of the positions from individual images, excluding any extreme spacecraft position model [1] and the camera pointing model [2], allow the outliers. This process used Spacecraft Position Kernels improved by LOLA precise determination of coordinates for those sites. Accurate knowledge of cross-over analysis and the GRAIL gravity model, with an uncertainty of the coordinates of spacecraft and spacecraft impact craters is critical for ±10 meters [1], and a temperature-corrected camera pointing model [2]. placing scientifc and engineering observations into their proper geologic At sites with a retrorefector in the same image as other objects (Apollo and geophysical context as well as completing the historic record of past 11, 14, and 15; Luna 17), we can improve the accuracy signifcantly. Since trips to the Moon. -
Voyage to Jupiter. INSTITUTION National Aeronautics and Space Administration, Washington, DC
DOCUMENT RESUME ED 312 131 SE 050 900 AUTHOR Morrison, David; Samz, Jane TITLE Voyage to Jupiter. INSTITUTION National Aeronautics and Space Administration, Washington, DC. Scientific and Technical Information Branch. REPORT NO NASA-SP-439 PUB DATE 80 NOTE 208p.; Colored photographs and drawings may not reproduce well. AVAILABLE FROMSuperintendent of Documents, U.S. Government Printing Office, Washington, DC 20402 ($9.00). PUB TYPE Reports - Descriptive (141) EDRS PRICE MF01/PC09 Plus Postage. DESCRIPTORS Aerospace Technology; *Astronomy; Satellites (Aerospace); Science Materials; *Science Programs; *Scientific Research; Scientists; *Space Exploration; *Space Sciences IDENTIFIERS *Jupiter; National Aeronautics and Space Administration; *Voyager Mission ABSTRACT This publication illustrates the features of Jupiter and its family of satellites pictured by the Pioneer and the Voyager missions. Chapters included are:(1) "The Jovian System" (describing the history of astronomy);(2) "Pioneers to Jupiter" (outlining the Pioneer Mission); (3) "The Voyager Mission"; (4) "Science and Scientsts" (listing 11 science investigations and the scientists in the Voyager Mission);.(5) "The Voyage to Jupiter--Cetting There" (describing the launch and encounter phase);(6) 'The First Encounter" (showing pictures of Io and Callisto); (7) "The Second Encounter: More Surprises from the 'Land' of the Giant" (including pictures of Ganymede and Europa); (8) "Jupiter--King of the Planets" (describing the weather, magnetosphere, and rings of Jupiter); (9) "Four New Worlds" (discussing the nature of the four satellites); and (10) "Return to Jupiter" (providing future plans for Jupiter exploration). Pictorial maps of the Galilean satellites, a list of Voyager science teams, and a list of the Voyager management team are appended. Eight technical and 12 non-technical references are provided as additional readings. -
Plasma Transport Into the Duskside Magnetopause Caused by Kelvin
https://doi.org/10.5194/angeo-2019-103 Preprint. Discussion started: 19 July 2019 c Author(s) 2019. CC BY 4.0 License. 1 Plasma transport into the duskside magnetopause caused by 2 Kelvin-Helmholtz vortices in response to the northward turning of 3 the interplanetary magnetic field observed by THEMIS 4 Guang Qing Yan1, George K. Parks2, Chun Lin Cai1, Tao. Chen1, James P. McFadden2, 5 Yong Ren1,3 6 1 State Key Laboratory of Space Weather, National Space Science Center, Chinese 7 Academy of Sciences, Beijing, China, 100190 8 2 Space Science Laboratory, University of California, Berkeley, California, USA, 9 CA94720 10 3 University of Chinese Academy of Sciences, Beijing, China, 100049 11 12 Abstract: A train of Kelvin-Helmholtz (K-H) vortices with plasma transport 13 across the magnetopause has been observed by the Time History of Events and 14 Macroscale Interactions during Substorms (THEMIS) when the interplanetary 15 magnetic field (IMF) abruptly turns northward. This unique event occurred 16 without pre-existing denser boundary layer to facilitate the instability. Two 17 THEMIS spacecraft, TH-A and TH-E, separated by 3 Re, periodically 18 encountered the duskside magnetopause and the low-latitude boundary layer 19 (LLBL) with a period of 2 minutes and tailward propagation of 194 km/s. There 20 was no high-velocity low-density feature, but the rotations in the bulk velocity 21 observation, distorted magnetopause with plasma parameter fluctuations and 22 the magnetic field line stretching, indicate the formation of rolled-up K-H 23 vortices at the duskside magnetopause. A mixture of magnetosheath ions with 24 magnetospheric ions and enhanced energy flux of hot electrons is identified in 25 the K-H vortices.