APL's Space Department After 40 Years: an Overview
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Key and Driving Requirements for the Juno Payload Suite of Instruments
Key and Driving Requirements for the Juno Payload Suite of Instruments Randy Dodge1 and Mark A. Boyles2 Jet Propulsion Laboratory-California Institute of Technology, Pasadena, CA, 91109-8099 Chuck E. Rasbach3 Lockheed Martin-Space System Company, Denver, CO, 80201 [Abstract] The Juno Mission was selected in the summer of 2005 via NASA’s New Frontiers competitive AO process (refer to http://www.nasa.gov/home/hqnews/2005/jun/HQ_05138_New_Frontiers_2.html). The Juno project is led by a Principle Investigator based at Southwest Research Institute [SwRI] in San Antonio, Texas, with project management based at the Jet Propulsion Laboratory [JPL] in Pasadena, California, while the Spacecraft design and Flight System integration are under contract to Lockheed Martin Space Systems Company [LM-SSC] in Denver, Colorado. The payload suite consists of a large number of instruments covering a wide spectrum of experimentation. The science team includes a lead Co-Investigator for each one of the following experiments: A Magnetometer experiment (consisting of both a FluxGate Magnetometer (FGM) built at Goddard Space Flight Center [GSFC] and a Scalar Helium Magnetometer (SHM) built at JPL, a MicroWave Radiometer (MWR) also built at JPL, a Gravity Science experiment (GS) implemented via the telecom subsystem, two complementary particle instruments (Jovian Auroral Distribution Experiment, JADE developed by SwRI and Juno Energetic-particle Detector Instrument, JEDI from the Applied Physics Lab [APL]--JEDI and JADE both measure electrons and ions), an Ultraviolet Spectrometer (UVS) also developed at SwRI, and a radio and plasma (Waves) experiment (from the University of Iowa). In addition, a visible camera (JunoCam) is included in the payload to facilitate education and public outreach (designed & fabricated by Malin Space Science Systems [MSSS]). -
University of Iowa Instruments in Space
University of Iowa Instruments in Space A-D13-089-5 Wind Van Allen Probes Cluster Mercury Earth Venus Mars Express HaloSat MMS Geotail Mars Voyager 2 Neptune Uranus Juno Pluto Jupiter Saturn Voyager 1 Spaceflight instruments designed and built at the University of Iowa in the Department of Physics & Astronomy (1958-2019) Explorer 1 1958 Feb. 1 OGO 4 1967 July 28 Juno * 2011 Aug. 5 Launch Date Launch Date Launch Date Spacecraft Spacecraft Spacecraft Explorer 3 (U1T9)58 Mar. 26 Injun 5 1(U9T68) Aug. 8 (UT) ExpEloxrpelro r1e r 4 1915985 8F eJbu.l y1 26 OEGxOpl o4rer 41 (IMP-5) 19697 Juunlye 2 281 Juno * 2011 Aug. 5 Explorer 2 (launch failure) 1958 Mar. 5 OGO 5 1968 Mar. 4 Van Allen Probe A * 2012 Aug. 30 ExpPloiorenre 3er 1 1915985 8M Oarc. t2. 611 InEjuxnp lo5rer 45 (SSS) 197618 NAouvg.. 186 Van Allen Probe B * 2012 Aug. 30 ExpPloiorenre 4er 2 1915985 8Ju Nlyo 2v.6 8 EUxpKlo 4r e(rA 4ri1el -(4IM) P-5) 197619 DJuenc.e 1 211 Magnetospheric Multiscale Mission / 1 * 2015 Mar. 12 ExpPloiorenre 5e r 3 (launch failure) 1915985 8A uDge.c 2. 46 EPxpiolonreeerr 4130 (IMP- 6) 19721 Maarr.. 313 HMEaRgCnIe CtousbpeShaetr i(cF oMxu-1ltDis scaatelell itMe)i ssion / 2 * 2021081 J5a nM. a1r2. 12 PionPeioenr e1er 4 1915985 9O cMt.a 1r.1 3 EExpxlpolorerer r4 457 ( S(IMSSP)-7) 19721 SNeopvt.. 1263 HMaalogSnaett oCsupbhee Sriact eMlluitlet i*scale Mission / 3 * 2021081 M5a My a2r1. 12 Pioneer 2 1958 Nov. 8 UK 4 (Ariel-4) 1971 Dec. 11 Magnetospheric Multiscale Mission / 4 * 2015 Mar. -
Book of Abstracts Ii Contents
2014 CAP Congress / Congrès de l’ACP 2014 Sunday, 15 June 2014 - Friday, 20 June 2014 Laurentian University / Université Laurentienne Book of Abstracts ii Contents An Analytic Mathematical Model to Explain the Spiral Structure and Rotation Curve of NGC 3198. .......................................... 1 Belle-II: searching for new physics in the heavy flavor sector ................ 1 The high cost of science disengagement of Canadian Youth: Reimagining Physics Teacher Education for 21st Century ................................. 1 What your advisor never told you: Education for the ’Real World’ ............. 2 Back to the Ionosphere 50 Years Later: the CASSIOPE Enhanced Polar Outflow Probe (e- POP) ............................................. 2 Changing students’ approach to learning physics in undergraduate gateway courses . 3 Possible Astrophysical Observables of Quantum Gravity Effects near Black Holes . 3 Supersymmetry after the LHC data .............................. 4 The unintentional irradiation of a live human fetus: assessing the likelihood of a radiation- induced abortion ...................................... 4 Using Conceptual Multiple Choice Questions ........................ 5 Search for Supersymmetry at ATLAS ............................. 5 **WITHDRAWN** Monte Carlo Field-Theoretic Simulations for Melts of Diblock Copoly- mer .............................................. 6 Surface tension effects in soft composites ........................... 6 Correlated electron physics in quantum materials ...................... 6 The -
Chapter 2 Tests of Magnetometer/Sun-Sensor Orbit Determination Using Flight Data*
Chapter 2 Tests of Magnetometer/Sun-Sensor Orbit Determination Using Flight Data* 2.1 Introduction Orbit determination is an old topic in celestial mechanics and is an essential part of satellite navigation. Traditional ground-based tracking methods that use range and range-rate measurements can provide an orbit accuracy as good as a few centimeters1. Autonomous orbit determination using only onboard measurements can be a requirement of military satellites in order to guarantee independence from ground facilities2. The rapid increase in the number of satellites also increases the need for autonomous navigation because of bottlenecks in ground tracking facilities3. A filter that uses magnetometer measurements provides one possible means of doing autonomous orbit determination. This idea was first introduced by Psiaki and Martel4 and has been tested by a number of researchers since then3,5-9. Magnetometers fly on most spacecraft (S/C) for attitude determination and control purposes. Therefore, successful autonomous orbit determination using magnetometer measurements can make the integration of attitude and orbit determination possible and lead to reduced mission costs. Although magnetometer-based autonomous orbit determination is unlikely to have better accuracy than ground-based tracking, a magnetometer-based system could be applied to a mission that does not need the accuracy of ground-station tracking. The Tropical Rainfall Measurement Mission * This chapter is from the published paper: Hee Jung and Mark L. Psiaki, “Tests of Magnetometer/Sun-Sensor Orbit Determination Using Flight Data,” Journal of Guidance, Control, and Dynamics, Volume 25, Number 3, pp. 582-590. [© 2002. The American Institute of Aeronautics and Astronautics, Inc]. 8 9 (TRMM), for example, requires 40 km position accuracy. -
Great Mambo Chicken and the Transhuman Condition
Tf Freewheel simply a tour « // o é Z oon" ‘ , c AUS Figas - 3 8 tion = ~ Conds : 8O man | S. | —§R Transhu : QO the Great Mambo Chicken and the Transhuman Condition Science Slightly Over the Edge ED REGIS A VV Addison-Wesley Publishing Company, Inc. - Reading, Massachusetts Menlo Park, California New York Don Mills, Ontario Wokingham, England Amsterdam Bonn Sydney Singapore Tokyo Madrid San Juan Paris Seoul Milan Mexico City Taipei Acknowledgmentof permissions granted to reprint previously published material appears on page 301. Manyofthe designations used by manufacturers andsellers to distinguish their products are claimed as trademarks. Where those designations appear in this book and Addison-Wesley was aware of a trademark claim, the designations have been printed in initial capital letters (e.g., Silly Putty). .Library of Congress Cataloging-in-Publication Data Regis, Edward, 1944— Great mambo chicken and the transhuman condition : science slightly over the edge / Ed Regis. p- cm. Includes bibliographical references. ISBN 0-201-09258-1 ISBN 0-201-56751-2 (pbk.) 1. Science—Miscellanea. 2. Engineering—Miscellanea. 3. Forecasting—Miscellanea. I. Title. Q173.R44 1990 500—dc20 90-382 CIP Copyright © 1990 by Ed Regis All rights reserved. No part ofthis publication may be reproduced, stored in a retrieval system, or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of the publisher. Printed in the United States of America. Text design by Joyce C. Weston Set in 11-point Galliard by DEKR Corporation, Woburn, MA - 12345678 9-MW-9594939291 Second printing, October 1990 First paperback printing, August 1991 For William Patrick Contents The Mania.. -
Juno Magnetometer (MAG) Standard Product Data Record and Archive Volume Software Interface Specification
Juno Magnetometer Juno Magnetometer (MAG) Standard Product Data Record and Archive Volume Software Interface Specification Preliminary March 6, 2018 Prepared by: Jack Connerney and Patricia Lawton Juno Magnetometer MAG Standard Product Data Record and Archive Volume Software Interface Specification Preliminary March 6, 2018 Approved: John E. P. Connerney Date MAG Principal Investigator Raymond J. Walker Date PDS PPI Node Manager Concurrence: Patricia J. Lawton Date MAG Ground Data System Staff 2 Table of Contents 1 Introduction ............................................................................................................................. 1 1.1 Distribution list ................................................................................................................... 1 1.2 Document change log ......................................................................................................... 2 1.3 TBD items ........................................................................................................................... 3 1.4 Abbreviations ...................................................................................................................... 4 1.5 Glossary .............................................................................................................................. 6 1.6 Juno Mission Overview ...................................................................................................... 7 1.7 Software Interface Specification Content Overview ......................................................... -
Space Weapons Earth Wars
CHILDREN AND FAMILIES The RAND Corporation is a nonprofit institution that EDUCATION AND THE ARTS helps improve policy and decisionmaking through ENERGY AND ENVIRONMENT research and analysis. HEALTH AND HEALTH CARE This electronic document was made available from INFRASTRUCTURE AND www.rand.org as a public service of the RAND TRANSPORTATION Corporation. INTERNATIONAL AFFAIRS LAW AND BUSINESS NATIONAL SECURITY Skip all front matter: Jump to Page 16 POPULATION AND AGING PUBLIC SAFETY SCIENCE AND TECHNOLOGY Support RAND Purchase this document TERRORISM AND HOMELAND SECURITY Browse Reports & Bookstore Make a charitable contribution For More Information Visit RAND at www.rand.org Explore RAND Project AIR FORCE View document details Limited Electronic Distribution Rights This document and trademark(s) contained herein are protected by law as indicated in a notice appearing later in this work. This electronic representation of RAND intellectual property is provided for non-commercial use only. Unauthorized posting of RAND electronic documents to a non-RAND website is prohibited. RAND electronic documents are protected under copyright law. Permission is required from RAND to reproduce, or reuse in another form, any of our research documents for commercial use. For information on reprint and linking permissions, please see RAND Permissions. The monograph/report was a product of the RAND Corporation from 1993 to 2003. RAND monograph/reports presented major research findings that addressed the challenges facing the public and private sectors. They included executive summaries, technical documentation, and synthesis pieces. SpaceSpace WeaponsWeapons EarthEarth WarsWars Bob Preston | Dana J. Johnson | Sean J.A. Edwards Michael Miller | Calvin Shipbaugh Project AIR FORCE R Prepared for the United States Air Force Approved for public release; distribution unlimited The research reported here was sponsored by the United States Air Force under Contract F49642-01-C-0003. -
Notice Should the Sun Become Unusually Exciting Plasma Instabilities by the Motion of the Active
N O T I C E THIS DOCUMENT HAS BEEN REPRODUCED FROM MICROFICHE. ALTHOUGH IT IS RECOGNIZED THAT CERTAIN PORTIONS ARE ILLEGIBLE, IT IS BEING RELEASED IN THE INTEREST OF MAKING AVAILABLE AS MUCH INFORMATION AS POSSIBLE _4^ M SOLAR TERREST RIA L PROGRAMS A. Five-Year Plan (NASA -TM- 82351) SOLAR TERRESTRIAL PROGRA MS; N81 -23992 A FIVE YEAR PLAN (NASA) 99 P HC A05/MF A01 CSCL 03B Unclas G3/92 24081 August 1978 ANN I ^ ^ Solar Terl &;;rraf Prugram5 Qtfic;e ~ `\^ Oft/ce of e Selanco,5 \ National A prcnautres and Space Administration ^• p;^f1 SOLAR TERRESTRIAL PROGRAMS A Five-Year Plan Prepared by 13,1-vd P. Stern Laboratory for Extraterrestrial Physiscs Goddard Space Flight Center, Greenbelt, Md. Solar Terrestrial Division Office of Space Sciences National Aeronautics and Space Administration "Perhaps the strongest area that we face now is the area of solar terrestrial interaction research, where we are still investigating it in a basic science sense: Clow doe the Sun work? What are all these cycles about? What do they have to .Jo with the Sun's magnetic field? Is the Sun a dynamo? What is happening to drive it in an energetic way? Why is it a, variable star to the extent to which it is variable, which is not very much, but enough to be troublesome to us? And what does all that mean in terms of structure? How does the Sun's radiation, either in a photon sense or a particle sense, the solar wind, affect the environment of the Earth, and does it have anything to do with the dynamics of the atmosphere? We have conic at that over centuries, in a sense, as a scientific problem, and we are working it as part of space science, and thinking of a sequence of missions in terms of space science. -
Initial Survey of the Wave Distribution Functions for Plasmaspheric Hiss
JOURNAL OF GEOPHYSICAL RESEARCH, VOL. 96, NO. All, PAGES 19,469-19,489, NOVEMBER 1, 1991 InitialSurvey of the Wave Distribution Functions for PlasmasphericHiss Observedby ISEE I L. R. O. S•o•s¾, • F . Lsrsvvgs, 2 M . PARROT,2 L . CAm6, • AND R. R. ANDERSON4 MulticomponentELF/VLF wavedata from the ISEE 1 satellitehave been analyzed with the aim of identifying the generationmechanism of plasmaspherichiss, and especiallyof determining whether it involveswave propagationon cyclictrajectories. The data were taken from four passes of the satellite, of which two were close to the geomagneticequatorial plane and two were farther from it; all four occurred during magnetically quiet periods. The principal method of analysis was calculation of the wave distribution functions. The waves appear to have been generated over a wide range of altitudes within the plasmasphere,and most, though not all, of them were propagating obliquely with respect to the Earth's magnetic field. On one of the passes near the equator, some wave energy was observed at small wave normal angles, and these waves may have been propagating on cyclic trajectories. Even here, however, obliquely propagating waves werepredominant, a finding that is difficultto reconcilewith the classicalquasi-linear generation mech•sm or its variants. The conclusion is that another mechanism, probably nonlinear, must have been generating most of the hiss observedon these four passes. 1. INTRODUCTION mals parallelto the field on the average[Smith et al., 1960; Plasmaspheric hiss is a broad-band and -
Atmosphere of Freedom: 70 Years at the NASA Ames Research Center
Atmosphere of Freedom: 70 Years at the NASA Ames Research Center 7 0 T H A N N I V E R S A R Y E D I T I O N G l e n n E . B u g o s National Aeronautics and Space Administration NASA History Office Washington, D.C. 2010 NASA SP-2010-4314 Table of Contents FOREWORD 1 PREFACE 3 A D M I N I S T R A T I V E H I S T O R Y DeFrance Aligns His Center with NASA 6 Harvey Allen as Director 13 Hans Mark 15 Clarence A. Syvertson 21 William F. Ballhaus, Jr. 24 Dale L. Compton 27 The Goldin Age 30 Moffett Field and Cultural Climate 33 Ken K. Munechika 37 Zero Base Review 41 Henry McDonald 44 G. Scott Hubbard 49 A Time of Transition 57 Simon “Pete” Worden 60 Once Again, Re-inventing NASA Ames 63 The Importance of Directors 71 S P A C E P R O J E C T S Spacecraft Program Management 76 Early Spaceflight Experiments 80 Pioneers 6 to 9 82 Magnetometers 85 Pioneers 10 and 11 86 Pioneer Venus 91 III Galileo Jupiter Probe 96 Lunar Prospector 98 Stardust 101 SOFIA 105 Kepler 110 LCROSS 117 Continuing Missions 121 E N G I N E E R I N G H U M A N S P A C E C R A F T “…returning him safely to earth” 125 Reentry Test Facilities 127 The Apollo Program 130 Space Shuttle Technology 135 Return To Flight 138 Nanotechology 141 Constellation 151 P L A N E T A R Y S C I E N C E S Impact Physics and Tektites 155 Planetary Atmospheres and Airborne Science 157 Infrared Astronomy 162 Exobiology and Astrochemistry 165 Theoretical Space Science 168 Search for Extraterrestrial Intelligence 171 Near-Earth Objects 173 NASA Astrobiology Institute 178 Lunar Science 183 S P A C E -
In-Orbit Aerodynamic Coefficient Measurements Using SOAR
In-Orbit Aerodynamic Coefficient Measurements using SOAR (Satellite for Orbital Aerodynamics Research) N.H. Crispa,, P.C.E. Robertsa, S. Livadiottia, A. Macario Rojasa, V.T.A. Oikoa, S. Edmondsona, S.J. Haigha, B.E.A. Holmesa, L.A. Sinpetrua, K.L. Smitha, J. Becedasb, R.M. Dom´ınguezb, V. Sulliotti-Linnerb, S. Christensenc, J. Nielsenc, M. Bisgaardc, Y-A. Chand, S. Fasoulasd, G.H. Herdrichd, F. Romanod, C. Traubd, D. Garc´ıa-Almi~nanae, S. Rodr´ıguez-Donairee, M. Suredae, D. Katariaf, B. Belkouchig, A. Conteg, S. Seminarig, R. Villaing aThe University of Manchester, Oxford Rd, Manchester, M13 9PL, United Kingdom bElecnor Deimos Satellite Systems, Calle Francia 9, 13500 Puertollano, Spain cGomSpace A/S, Langagervej 6, 9220 Aalborg East, Denmark dInstitute of Space Systems (IRS), University of Stuttgart, Pfaffenwaldring 29, 70569 Stuttgart, Germany eUPC-BarcelonaTECH, Carrer de Colom 11, 08222 Terrassa, Barcelona, Spain fMullard Space Science Laboratory, University College London, Holmbury St. Mary, Dorking, RH5 6NT, United Kingdom gEuroconsult, 86 Boulevard de S´ebastopol, 75003 Paris, France Abstract The Satellite for Orbital Aerodynamics Research (SOAR) is a CubeSat mission, due to be launched in 2021, to investigate the interaction between different materials and the atmospheric flow regime in very low Earth orbits (VLEO). Improving knowledge of the gas-surface interactions at these altitudes and identification of novel materials that can minimise drag or improve aerodynamic control are important for the design of future spacecraft that can operate in lower altitude orbits. Such satellites may be smaller and cheaper to develop or can provide improved Earth observation data or communications link-budgets and latency. -
Planet Mars III 28 March- 2 April 2010 POSTERS: ABSTRACT BOOK
Planet Mars III 28 March- 2 April 2010 POSTERS: ABSTRACT BOOK Recent Science Results from VMC on Mars Express Jonathan Schulster1, Hannes Griebel2, Thomas Ormston2 & Michel Denis3 1 VCS Space Engineering GmbH (Scisys), R.Bosch-Str.7, D-64293 Darmstadt, Germany 2 Vega Deutschland Gmbh & Co. KG, Europaplatz 5, D-64293 Darmstadt, Germany 3 Mars Express Spacecraft Operations Manager, OPS-OPM, ESA-ESOC, R.Bosch-Str 5, D-64293, Darmstadt, Germany. Mars Express carries a small Visual Monitoring Camera (VMC), originally to provide visual telemetry of the Beagle-2 probe deployment, successfully release on 19-December-2003. The VMC comprises a small CMOS optical camera, fitted with a Bayer pattern filter for colour imaging. The camera produces a 640x480 pixel array of 8-bit intensity samples which are recoded on ground to a standard digital image format. The camera has a basic command interface with almost all operations being performed at a hardware level, not featuring advanced features such as patchable software or full data bus integration as found on other instruments. In 2007 a test campaign was initiated to study the possibility of using VMC to produce full disc images of Mars for outreach purposes. An extensive test campaign to verify the camera’s capabilities in-flight was followed by tuning of optimal parameters for Mars imaging. Several thousand images of both full- and partial disc have been taken and made immediately publicly available via a web blog. Due to restrictive operational constraints the camera cannot be used when any other instrument is on. Most imaging opportunities are therefore restricted to a 1 hour period following each spacecraft maintenance window, shortly after orbit apocenter.