Solar Parameters for Modeling Interplanetary Background
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IBM Explorer for Z/OS: Host Configuration Reference Guide RSE Daemon and Thread Pool Logging
IBM Explorer for z/OS IBM Host Configuration Reference Guide SC27-8438-02 IBM Explorer for z/OS IBM Host Configuration Reference Guide SC27-8438-02 Note Before using this information, be sure to read the general information under “Notices” on page 175. Third edition (September, 2017) This edition applies to IBM Explorer for z/OS Version 3.1.1 (program number 5655-EX1) and to all subsequent releases and modifications until otherwise indicated in new editions. © Copyright IBM Corporation 2017. US Government Users Restricted Rights – Use, duplication or disclosure restricted by GSA ADP Schedule Contract with IBM Corp. Contents Figures .............. vii Certificate Authority (CA) validation ..... 24 (Optional) Query a Certificate Revocation List Tables ............... ix (CRL) ............... 25 Authentication by your security software ... 25 Authentication by RSE daemon....... 26 About this document ......... xi Port Of Entry (POE) checking ........ 27 Who should use this document ........ xi Altering client functions .......... 27 Description of the document content ...... xi OFF.REMOTECOPY.MVS ......... 28 Understanding z/OS Explorer ....... xii Push-to-client developer groups ....... 28 Security considerations ......... xii Send message security........... 30 TCP/IP considerations ......... xii Log file security ............. 31 WLM considerations .......... xii UNIXPRIV class permits.......... 32 Tuning considerations .......... xii BPX.SUPERUSER profile permit ....... 33 Performance considerations ........ xii UID 0 ............... 33 Push-to-client considerations ....... xii Miscellaneous information ......... 33 User exit considerations ......... xii GATE trashing ............ 33 Customizing the TSO environment ..... xiii Managed ACEE ............ 33 Troubleshooting configuration problems ... xiii ACEE caching ............ 34 Setting up encrypted communication and X.509 TCP/IP port reservation ......... 34 authentication ............ xiii z/OS Explorer configuration files ....... 34 Setting up TCP/IP........... xiii JES Job Monitor - FEJJCNFG....... -
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. -
Information Summaries
TIROS 8 12/21/63 Delta-22 TIROS-H (A-53) 17B S National Aeronautics and TIROS 9 1/22/65 Delta-28 TIROS-I (A-54) 17A S Space Administration TIROS Operational 2TIROS 10 7/1/65 Delta-32 OT-1 17B S John F. Kennedy Space Center 2ESSA 1 2/3/66 Delta-36 OT-3 (TOS) 17A S Information Summaries 2 2 ESSA 2 2/28/66 Delta-37 OT-2 (TOS) 17B S 2ESSA 3 10/2/66 2Delta-41 TOS-A 1SLC-2E S PMS 031 (KSC) OSO (Orbiting Solar Observatories) Lunar and Planetary 2ESSA 4 1/26/67 2Delta-45 TOS-B 1SLC-2E S June 1999 OSO 1 3/7/62 Delta-8 OSO-A (S-16) 17A S 2ESSA 5 4/20/67 2Delta-48 TOS-C 1SLC-2E S OSO 2 2/3/65 Delta-29 OSO-B2 (S-17) 17B S Mission Launch Launch Payload Launch 2ESSA 6 11/10/67 2Delta-54 TOS-D 1SLC-2E S OSO 8/25/65 Delta-33 OSO-C 17B U Name Date Vehicle Code Pad Results 2ESSA 7 8/16/68 2Delta-58 TOS-E 1SLC-2E S OSO 3 3/8/67 Delta-46 OSO-E1 17A S 2ESSA 8 12/15/68 2Delta-62 TOS-F 1SLC-2E S OSO 4 10/18/67 Delta-53 OSO-D 17B S PIONEER (Lunar) 2ESSA 9 2/26/69 2Delta-67 TOS-G 17B S OSO 5 1/22/69 Delta-64 OSO-F 17B S Pioneer 1 10/11/58 Thor-Able-1 –– 17A U Major NASA 2 1 OSO 6/PAC 8/9/69 Delta-72 OSO-G/PAC 17A S Pioneer 2 11/8/58 Thor-Able-2 –– 17A U IMPROVED TIROS OPERATIONAL 2 1 OSO 7/TETR 3 9/29/71 Delta-85 OSO-H/TETR-D 17A S Pioneer 3 12/6/58 Juno II AM-11 –– 5 U 3ITOS 1/OSCAR 5 1/23/70 2Delta-76 1TIROS-M/OSCAR 1SLC-2W S 2 OSO 8 6/21/75 Delta-112 OSO-1 17B S Pioneer 4 3/3/59 Juno II AM-14 –– 5 S 3NOAA 1 12/11/70 2Delta-81 ITOS-A 1SLC-2W S Launches Pioneer 11/26/59 Atlas-Able-1 –– 14 U 3ITOS 10/21/71 2Delta-86 ITOS-B 1SLC-2E U OGO (Orbiting Geophysical -
Asa R-/ 130090
rl),,; ASA R-/130090 The University of Texas at Dallas Final Technical Report NASA Contract NAS 5-9075 on Measurement of the Degree of Anisotropy of the Cosmic Radiation Using the IMP Space Vehicle by R. A. R. Palmeira and F. R. Allum The University of Texas at Dallas Dallas, Texas This report was prepared for submission to NASA/Goddard Space Flight Center in partial fulfillment of the terms of the Contract NAS 5-9075. October 1972 (NASA-CR-130090 ) MEASUREMENT OF THE DEGREE N72-3376 OF ANISOTROPY OF THE COSMIC RADIATION USING 8 THE IMP SPACE VEHICLE Final Technical Report R.A.R. Palmeira, et al (Texas Unclas Univ.) Oct. 1972 31 p CSCL 03B G3/29 45262 The University of Texas at Dallas Final Technical Report on "Measurement of the Degree of Anisotropy of the Cosmic Radiation Using the IMP Space Vehicle" NASA Contract NAS 5-9075 by R.A.R. Palmeira and F. R. Allum The University of Texas at Dallas, Dallas, Texas INTRODUCTION This report describes the detector and data reduction techniques used in connection with the UTD cosmic-ray experiments designed for and flown on board the Explorer 34 and 41 satellites. It is intended to supplement and summarize the more detailed information supplied during the course of the program, including but not restricted to the information contained in the contractually required Monthly Technical Reports submitted throughout the duration of the program. This final technical report is divided into three categories: i) a brief history of the UTD program development; ii) a description of the particle detectors and the methods of data analysis; and iii) present status of data processing. -
Photographs Written Historical and Descriptive
CAPE CANAVERAL AIR FORCE STATION, MISSILE ASSEMBLY HAER FL-8-B BUILDING AE HAER FL-8-B (John F. Kennedy Space Center, Hanger AE) Cape Canaveral Brevard County Florida PHOTOGRAPHS WRITTEN HISTORICAL AND DESCRIPTIVE DATA HISTORIC AMERICAN ENGINEERING RECORD SOUTHEAST REGIONAL OFFICE National Park Service U.S. Department of the Interior 100 Alabama St. NW Atlanta, GA 30303 HISTORIC AMERICAN ENGINEERING RECORD CAPE CANAVERAL AIR FORCE STATION, MISSILE ASSEMBLY BUILDING AE (Hangar AE) HAER NO. FL-8-B Location: Hangar Road, Cape Canaveral Air Force Station (CCAFS), Industrial Area, Brevard County, Florida. USGS Cape Canaveral, Florida, Quadrangle. Universal Transverse Mercator Coordinates: E 540610 N 3151547, Zone 17, NAD 1983. Date of Construction: 1959 Present Owner: National Aeronautics and Space Administration (NASA) Present Use: Home to NASA’s Launch Services Program (LSP) and the Launch Vehicle Data Center (LVDC). The LVDC allows engineers to monitor telemetry data during unmanned rocket launches. Significance: Missile Assembly Building AE, commonly called Hangar AE, is nationally significant as the telemetry station for NASA KSC’s unmanned Expendable Launch Vehicle (ELV) program. Since 1961, the building has been the principal facility for monitoring telemetry communications data during ELV launches and until 1995 it processed scientifically significant ELV satellite payloads. Still in operation, Hangar AE is essential to the continuing mission and success of NASA’s unmanned rocket launch program at KSC. It is eligible for listing on the National Register of Historic Places (NRHP) under Criterion A in the area of Space Exploration as Kennedy Space Center’s (KSC) original Mission Control Center for its program of unmanned launch missions and under Criterion C as a contributing resource in the CCAFS Industrial Area Historic District. -
Profit Embedded PHD : Process Trend User's Guide
Uniformance 160 Process Trend (Profit Embedded PHD) User's Guide Uniformance 160 Process Trend (Profit Embedded PHD) User's Guide Copyright, Notices, and Trademarks Copyright, Notices, and Trademarks © Honeywell Inc. 1998 – 2001. All Rights Reserved. Release 160 – March 30, 2001 While this information is presented in good faith and believed to be accurate, Honeywell disclaims the implied warranties of merchantability and fitness for a particular purpose and makes no express warranties except as may be stated in its written agreement with and for its customers. In no event is Honeywell liable to anyone for any indirect, special or consequential damages. The information and specifications in this document are subject to change without notice. Honeywell, TotalPlant, Uniformance, and Business.FLEX are U.S. registered trademarks of Honeywell Inc. Other brand or product names are trademarks of their respective owners. Release Information Uniformance 160 Revision: 1 Revision Date: April 2001 Document Number: AP20-530PS Honeywell Inc. Industrial Automation and Control Automation College 2500 West Union Hills Drive Phoenix, AZ, 85027 ii • Uniformance Process Trend User Guide Contents Contents Copyright, Notices, and Trademarks ii Release Information ii Contents iii About Process Trend 9 Overview 9 About this Guide 10 Who Should Use this Guide 10 What's in this Guide 10 Conventions Used in this Guide 11 Contact Us 11 Getting Started 13 System Requirements 13 Starting Process Trend 13 Logging into Process Trend 13 Bypassing the PHD Login 14 Saving -
Deep Space Chronicle Deep Space Chronicle: a Chronology of Deep Space and Planetary Probes, 1958–2000 | Asifa
dsc_cover (Converted)-1 8/6/02 10:33 AM Page 1 Deep Space Chronicle Deep Space Chronicle: A Chronology ofDeep Space and Planetary Probes, 1958–2000 |Asif A.Siddiqi National Aeronautics and Space Administration NASA SP-2002-4524 A Chronology of Deep Space and Planetary Probes 1958–2000 Asif A. Siddiqi NASA SP-2002-4524 Monographs in Aerospace History Number 24 dsc_cover (Converted)-1 8/6/02 10:33 AM Page 2 Cover photo: A montage of planetary images taken by Mariner 10, the Mars Global Surveyor Orbiter, Voyager 1, and Voyager 2, all managed by the Jet Propulsion Laboratory in Pasadena, California. Included (from top to bottom) are images of Mercury, Venus, Earth (and Moon), Mars, Jupiter, Saturn, Uranus, and Neptune. The inner planets (Mercury, Venus, Earth and its Moon, and Mars) and the outer planets (Jupiter, Saturn, Uranus, and Neptune) are roughly to scale to each other. NASA SP-2002-4524 Deep Space Chronicle A Chronology of Deep Space and Planetary Probes 1958–2000 ASIF A. SIDDIQI Monographs in Aerospace History Number 24 June 2002 National Aeronautics and Space Administration Office of External Relations NASA History Office Washington, DC 20546-0001 Library of Congress Cataloging-in-Publication Data Siddiqi, Asif A., 1966 Deep space chronicle: a chronology of deep space and planetary probes, 1958-2000 / by Asif A. Siddiqi. p.cm. – (Monographs in aerospace history; no. 24) (NASA SP; 2002-4524) Includes bibliographical references and index. 1. Space flight—History—20th century. I. Title. II. Series. III. NASA SP; 4524 TL 790.S53 2002 629.4’1’0904—dc21 2001044012 Table of Contents Foreword by Roger D. -
UNIVERSITY of CALIFORNIA Los Angeles Charged
UNIVERSITY OF CALIFORNIA Los Angeles Charged Particle Energization and Transport in the Magnetotail during Substorms A dissertation submitted in partial satisfaction of the requirements for the degree Doctor of Philosophy in Physics by Qingjiang Pan 2015 ABSTRACT OF THE DISSERTATION Charged Particle Energization and Transport in the Magnetotail during Substorms by Qingjiang Pan Doctor of Philosophy in Physics University of California, Los Angeles, 2015 Professor Maha Ashour-Abdalla, Chair This dissertation addresses the problem of energization of particles (both electrons and ions) to tens and hundreds of keV and the associated transport process in the magnetotail during substorms. Particles energized in the magnetotail are further accelerated to even higher energies (hundreds of keV to MeV) in the radiation belts, causing space weather hazards to human activities in space and on ground. We develop an analytical model to quantitatively estimate flux changes caused by betatron and Fermi acceleration when particles are transported along narrow high-speed flow channels from the magnetotail to the inner magnetosphere. The model shows that energetic particle flux can be significantly enhanced by a modest compression of the magnetic field and/or ii shrinking of the distance between the magnetic mirror points. We use coordinated spacecraft measurements, global magnetohydrodynamic (MHD) simulations driven by measured upstream solar wind conditions, and large-scale kinetic (LSK) simulations to quantify electron local acceleration in the near-Earth reconnection region and nonlocal acceleration during plasma earthward transport. Compared to the analytical model, application of the LSK simulations is much less restrictive because trajectories of millions of test particles are calculated in the realistically determined global MHD fields and the results are statistical. -
ISEE&Hyphen;3 Wave Measurements in the Distant Geomagnetic Tail And
GEOPHYSICALRESEARCH LETTERS, VOL. 11, NO. 4, PAGES335-338, APRIL 1984 ISEE-3 WAVE MEASUREMENTS IN THE DISTANT GEOMAGNETIC TAIL AND BOUNDARY LAYER Fß L. Scarfl , F. V. Coroniti1, Cß F. KennelI , Rß Wß Fredricks1 D. A. Gurnett2, andE ß Jß Smith3 1TRWSpace and Technology Group, Redondo Beach, California 90278 2Universityof Iowa,Iowa City, Iowa 52242 3jet PropulsionLaboratory, Pasadena, California 91109 Abstractß The ISEE-3 excursion into the dis- field configuration for the first relatively tant tail region reveals a complex structure with close-in traversal of the tail (r < 94 Re) and several wave, particle and field characteristics for the first deep excursion to r = 225 Re. In that differ significantly from those measured another recent report, Bame et al. (1983) pre- closer to earth. The most striking results are Sented initial results from the ISEE-3 plasma found within the distant boundary layer where in- analyzer, and they showed that all plasma regimes tense electrostatic turbulence levels are de- identified from earlier measurements (plasma tected in association with bi-directional elec- sheet, low latitude boundary levels, mantle, lobe tron distributions. The wave amplitudes appear and magnetosheath) remained recognizable in the to increase with increasing downstream distance distant tail, although the regimes appeared to be and the polarizations are those expected for ion "intermingled" far from earth, and a well-defined acoustic oscillations. Near the boundary of the low density tail lobe was rarely encountered. distant plasmas sheet the turbulence spectra are The distant tail plasma was also characterized by essentially identical to those measured much unusually large flow speeds (generally tailward) closer to earth on IMP-8. -
ESRO SP-72 European Space Research Organisation
ESRO SP-72 I. Proc. ESRO-GRI ESRO SP-72 I. Proc ESRO-GRI European Space Research Organisation Colloquium March 1971 European Space Research Organisation Colloquium March 1971 COLLOQUIUM ON WAVE-PARTICLE INTER II. ESRO SP-72 COLLOQUIUM ON WAVE-PARTICLE INTER II. ESRO SP-72 ACTIONS IN THE MAGNETOSPHERE HI. Texts in English ACTIONS IN THE MAGNETOSPHERE III. Texts in English September 1971 September 1971 iv + 284 pages iv + 284 pages The Colloquium on wave-particle interactions in the magnetosphere held in The Colloquium on wave-particle interactions in the magnetosphere held in Orleans (March 17-19,1971) intended to review the outstanding problems still unsolved Orleans (March 17-19, 1971) intended to review the outstanding problems still unsolved in this field : in this field : — large-scale dynamics of the magnetosphere; — large-scale dynamics of the magnetosphere; — distribution of 'Oasma parameters; — distribution of plasma parameters; — decoupling of n..gnetospheric from ionospheric plasma; — decoupling of magnetospheric from ionospheric plasma; — acceleration and convection mechanisms; — acceleration and convection mechanisms; — substorms; — substorms; — polar wind..., — polar wind..., as well as the theoretical and experimental work needed to solve these problems in the as well as the theoretical and experimental work needed to solve these problems in the light of previous experiments (rocket launchings in auroral zone, Ariel 3 satellite...) light of previous experiments (rocket launchings in auroral zone, Ariel 3 satellite...) and of technical achievements (onboard computers, new sensors...). and of technical achievements (onboard computers, new sensors...). Ensuing discussions attempted to define types of missions which could be carried Ensuing discussions attempted to define types of missions which could be carried out in the future by the Small Scientific Satellites now being considered by ESRO. -
Do Statistical Models Capture the Dynamics of the Magnetopause
manuscript submitted to JGR: Space Physics 1 Do statistical models capture the dynamics of the 2 magnetopause during sudden magnetospheric 3 compressions? 1 1 1 2 3 4 F. A. Staples , I. J. Rae , C. Forsyth , A. R. A. Smith , K.R. Murphy , K. 4 5 6 7 6 5 M. Raymer , F. Plaschke , N. A. Case , C. J. Rodger , J. A. Wild , S. E. 4 4 6 Milan , S. M. Imber 1 7 Mullard Space Science Laboratory, University College London, London, UK 2 8 School of GeoSciences, University of Edinburgh, Edinburgh, UK 3 9 NASA Goddard Space Flight Centre, Greenbelt, MD, USA 4 10 Department of Physics and Astronomy, University of Leicester, Leicester, UK 5 11 Space Research Institute, Austrian Academy of Sciences, Graz, Austria. 6 12 Department of Physics, Lancaster University, Lancaster, UK 7 13 Department of Physics, University of Otago, Dunedin, New Zealand 14 Key Points: 15 • Measured magnetopause location is statistically closer to the Earth than Shue et 16 al. (1998) modelled for storm sudden commencements (SYM-H ≥ 15 nT). 17 • When the magnetopause is compressed below 8 RE, the average measured loca- 18 tion is > 1 RE inside of the Shue et al. (1998) model location. 19 • Extreme magnetopause compressions rarely reach the outer radiation belt, there- 20 fore rapid outward radial transport is required to fully explain most shadowing 21 events. Corresponding author: Frances A. Staples, [email protected] {1{ manuscript submitted to JGR: Space Physics 22 Abstract 23 Under periods of strong solar wind driving, the magnetopause can become compressed, 24 playing a significant role in draining electrons from the outer radiation belt. -
A Y' 1969-Deeber 1972
- -7 5, 41, AN MA 969-DECEMBER43 D 47 197 AY' 1969-DEEBER 1972 S(NASA-TM-X-70481) TRAJECTORIES OF N73-33809 EXPLORERS 33, 35, 41, 43 AND 47, MAY 1969 - DEC. 1972 (NASA) 72 p HC $5.75 CSCL 22C Unclas "f -" G3/30 19441 D.' -'.FAIRFIELD K. W. BEAANNON( R. P LEPPING N. F. NESS "NFORMATN SERVI-E i -- SSpringfield, _ e te. VA.o Com 22151 e 1 AR -SPAC FLIGHT CETER S-ENBET MA RYLAND -N 14 N- TRAJECTORIES OF EXPLORERS 33, 35, 41, 43 and 47 May 1969-Dec 1972 D.H. Fairfield K.W. Behannon R.P. Lepping N.F. Ness Laboratory for Extraterrestrial Physics Goddard Space Flight Center Greenbelt, Maryland October 1973 /0 This document represents a continuation of a previous document (Behannon et al. 1970) and is presented with the intention that it will stimulate and facilitate correlative studies of data from various spacecraft. Figures 1-54 consist primarily of solar ecliptic plane projections of orbits of five different satellites although a limited number of XZ projections are shown to illustrate the large excursions of Explorer 33 away from the ecliptic plane. Nominal positions of the magnetopause and bow shock are included for reference. The plots are intended only to represent the trajectory of the spacecraft and imply nothing about the operational status of the various experiments nor the availability of the data. Information on these latter points can be ob- tained from the National Space Science Data Center, (e.g. King, 1971). It should be pointed out, however, that Explorers33 and 35 were very long lived spacecraft (> 2 yrs) and numerous experiments either ceased operation or exhibited a gradual deterioration during the extended lifetime.