ESRO SP-72 European Space Research Organisation
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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....... -
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. -
ARIEL – 13Th Appleton Space Conference PLANETS ARE UBIQUITOUS
Background image credit NASA ARIEL – 13th Appleton Space Conference PLANETS ARE UBIQUITOUS OUR GALAXY IS MADE OF GAS, STARS & PLANETS There are at least as many planets as stars Cassan et al, 2012; Batalha et al., 2015; ARIEL – 13th Appleton Space Conference 2 EXOPLANETS TODAY: HUGE DIVERSITY 3700+ PLANETS, 2700 PLANETARY SYSTEMS KNOWN IN OUR GALAXY ARIEL – 13th Appleton Space Conference 3 HUGE DIVERSITY: WHY? FORMATION & EVOLUTION PROCESSES? MIGRATION? INTERACTION WITH STAR? Accretion Gaseous planets form here Interaction with star Planet migration Ices, dust, gas ARIEL – 13th Appleton Space Conference 4 STAR & PLANET FORMATION/EVOLUTION WHAT WE KNOW: CONSTRAINTS FROM OBSERVATIONS – HERSCHEL, ALMA, SOLAR SYSTEM Measured elements in Solar system ? Image credit ESA-Herschel, ALMA (ESO/NAOJ/NRAO), Marty et al, 2016; André, 2012; ARIEL – 13th Appleton Space Conference 5 THE SUN’S PLANETS ARE COLD SOME KEY O, C, N, S MOLECULES ARE NOT IN GAS FORM T ~ 150 K Image credit NASA Juno mission, NASA Galileo ARIEL – 13th Appleton Space Conference 6 WARM/HOT EXOPLANETS O, C, N, S (TI, VO, SI) MOLECULES ARE IN GAS FORM Atmospheric pressure 0.01Bar H2O gas CO2 gas CO gas CH4 gas HCN gas TiO gas T ~ 500-2500 K Condensates VO gas H2S gas 1 Bar Gases from interior ARIEL – 13th Appleton Space Conference 7 CHEMICAL MEASUREMENTS TODAY SPECTROSCOPIC OBSERVATIONS WITH CURRENT INSTRUMENTS (HUBBLE, SPITZER,SPHERE,GPI) • Precision of 20 ppm can be reached today by Hubble-WFC3 • Current data are sparse, instruments not absolutely calibrated • ~ 40 planets analysed -
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 -
Solar Parameters for Modeling Interplanetary Background
— 2 — Solar parameters for modeling interplanetary background M. Bzowski, J.M. Sokoł´ Space Research Center Polish Academy of Sciences, Warsaw, Poland M. Tokumaru,K.Fujiki Solar-Terrestrial Environment Laboratory, Nagoya University, Nagoya, Japan E. Quemerais,R.Lallement LATMOS-IPSL, Universite Versailles Saint-Quentin, Guyancourt, France S. Ferron ACRI-ST, Sophia Antipolis, France P. Bochsler Space Science Center & Department of Physics, University of New Hampshire, Durham NH Physikalisches Institut, University of Bern, Bern, Switzerland D.J. McComas Southwest Research Institute, San Antonio TX University of Texas at San Antonio, San Antonio, TX 78249, USA Abstract The goal of the Fully Online Datacenter of Ultraviolet Emissions (FONDUE) Work- ing Team of the International Space Science Institute (ISSI) in Bern, Switzerland, was to establish a common calibration of various UV and EUV heliospheric observations, both spectroscopic and photometric. Realization of this goal required a credible and up-to-date model of spatial distribution of neutral interstellar hydrogen in the heliosphere, and to that end, a credible model of the radiation pressure and ionization processes was needed. This chapter describes the latter part of the project: the solar factors responsible for shap- arXiv:1112.2967v1 [astro-ph.SR] 13 Dec 2011 ing the distribution of neutral interstellar H in the heliosphere. Presented are the solar Lyman-alpha flux and the question of solar Lyman-alpha resonant radiation pressure force acting on neutral H atoms in the heliosphere, solar EUV radiation and the process of pho- toionization of heliospheric hydrogen, and their evolution in time and the still hypothetical variation with heliolatitude. Further, solar wind and its evolution with solar activity is 1 2 2. -
Table of Artificial Satellites Launched Between 1 January and 31 December 1967
This electronic version (PDF) was scanned by the International Telecommunication Union (ITU) Library & Archives Service from an original paper document in the ITU Library & Archives collections. La présente version électronique (PDF) a été numérisée par le Service de la bibliothèque et des archives de l'Union internationale des télécommunications (UIT) à partir d'un document papier original des collections de ce service. Esta versión electrónica (PDF) ha sido escaneada por el Servicio de Biblioteca y Archivos de la Unión Internacional de Telecomunicaciones (UIT) a partir de un documento impreso original de las colecciones del Servicio de Biblioteca y Archivos de la UIT. (ITU) ﻟﻼﺗﺼﺎﻻﺕ ﺍﻟﺪﻭﻟﻲ ﺍﻻﺗﺤﺎﺩ ﻓﻲ ﻭﺍﻟﻤﺤﻔﻮﻇﺎﺕ ﺍﻟﻤﻜﺘﺒﺔ ﻗﺴﻢ ﺃﺟﺮﺍﻩ ﺍﻟﻀﻮﺋﻲ ﺑﺎﻟﻤﺴﺢ ﺗﺼﻮﻳﺮ ﻧﺘﺎﺝ (PDF) ﺍﻹﻟﻜﺘﺮﻭﻧﻴﺔ ﺍﻟﻨﺴﺨﺔ ﻫﺬﻩ .ﻭﺍﻟﻤﺤﻔﻮﻇﺎﺕ ﺍﻟﻤﻜﺘﺒﺔ ﻗﺴﻢ ﻓﻲ ﺍﻟﻤﺘﻮﻓﺮﺓ ﺍﻟﻮﺛﺎﺋﻖ ﺿﻤﻦ ﺃﺻﻠﻴﺔ ﻭﺭﻗﻴﺔ ﻭﺛﻴﻘﺔ ﻣﻦ ﻧﻘﻼ ً◌ 此电子版(PDF版本)由国际电信联盟(ITU)图书馆和档案室利用存于该处的纸质文件扫描提供。 Настоящий электронный вариант (PDF) был подготовлен в библиотечно-архивной службе Международного союза электросвязи путем сканирования исходного документа в бумажной форме из библиотечно-архивной службы МСЭ. © International Telecommunication Union HIS list of artificial satellites launched in 1967 was prepared from information provided by TTelecommunication Administrations, the Com m ittee on Space Research (COSPAR), the Goddard Space Flight Center (GSFC), the United States National Aeronautics and Space Administration (NASA), the International Fre quency Registration Board (IFRB), one of the fo ur permanent organs o f the ITU, and from details published in the specialized press. For decayed satellites the data concerning the orbit parameters are those immediately after launching. For the others, still in orbit, the orbit parameters are those reported on 31 De cember 1967 by GSFC. -
ESWW7 Abstract Book.Pdf
2 Table of Contents Committees ......................................................................................................................................................4 Sponsors ...........................................................................................................................................................5 Programme Monday, 15 November 2010...............................................................................................................6 Tuesday, 16 November 2010...............................................................................................................9 Wednesday, 17 November 2010 .......................................................................................................11 Thursday, 18 November 2010 ...........................................................................................................13 Friday, 19 November 2010 ................................................................................................................15 Poster Sessions ..................................................................................................................................17 Abstracts.........................................................................................................................................................25 3 Committees Programme Committee A. Belehaki (Co‐Chair, NOA & COST ES0803) A. Glover (Co‐Chair, ESA) M. Hapgood (RAL/STFC, SWWT) J.‐P. Luntama (ESA) R. Van der Linden (SIDC‐STCE) P. Vanlommel (STCE) T. -
Electron Density Profiles of the Topside Ionosphere
ANNALS OF GEOPHYSICS, VOL. 45, N. 1, February 2002 Electron density profiles of the topside ionosphere Xueqin Huang (1), Bodo W. Reinisch (1), Dieter Bilitza (2) and Robert F. Benson (3) (1) Center for Atmospheric Research, University of Massachusetts Lowell, MA, U.S.A. (2) Raytheon ITSS, GSFC, Code 632, Greenbelt, MD, U.S.A. (3) GSFC, Code 692, Greenbelt, MD, U.S.A. Abstract The existing uncertainties about the electron density profiles in the topside ionosphere, i.e., in the height region from hmF2 to ~ 2000 km, require the search for new data sources. The ISIS and Alouette topside sounder satellites from the sixties to the eighties recorded millions of ionograms but most were not analyzed in terms of electron density profiles. In recent years an effort started to digitize the analog recordings to prepare the ionograms for computerized analysis. As of November 2001 about 350 000 ionograms have been digitized from the original 7-track analog tapes. These data are available in binary and CDF format from the anonymous ftp site of the National Space Science Data Center. A search site and browse capabilities on CDAWeb assist the scientific usage of these data. All information and access links can be found at http://nssdc.gsfc.nasa.gov/space/isis/isis- status.html. This paper describes the ISIS data restoration effort and shows how the digital ionograms are automatically processed into electron density profiles from satellite orbit altitude (1400 km for ISIS-2) down to the F peak. Because of the large volume of data an automated processing algorithm is imperative. -
Radiation Belt Storm Probes Ion Composition Experiment (RBSPICE)
Space Sci Rev DOI 10.1007/s11214-013-9965-x Radiation Belt Storm Probes Ion Composition Experiment (RBSPICE) D.G. Mitchell · L.J. Lanzerotti · C.K. Kim · M. Stokes · G. Ho · S. Cooper · A. Ukhorskiy · J.W. Manweiler · S. Jaskulek · D.K. Haggerty · P. Brandt · M. Sitnov · K. Keika · J.R. Hayes · L.E. Brown · R.S. Gurnee · J.C. Hutcheson · K.S. Nelson · N. Paschalidis · E. Rossano · S. Kerem Received: 30 June 2012 / Accepted: 1 February 2013 © The Author(s) 2013. This article is published with open access at Springerlink.com Abstract The Radiation Belt Storm Probes Ion Composition Experiment (RBSPICE) on the two Van Allen Probes spacecraft is the magnetosphere ring current instrument that will provide data for answering the three over-arching questions for the Van Allen Probes Pro- gram: RBSPICE will determine “how space weather creates the storm-time ring current around Earth, how that ring current supplies and supports the creation of the radiation belt populations,” and how the ring current is involved in radiation belt losses. RBSPICE is a time-of-flight versus total energy instrument that measures ions over the energy range from ∼20 keV to ∼1 MeV. RBSPICE will also measure electrons over the energy range ∼25 keV to ∼1 MeV in order to provide instrument background information in the radiation belts. A description of the instrument and its data products are provided in this chapter. Keywords Magnetosphere · Ring current · Time-of-flight · Radiation belt · Space weather 1 Introduction The idea, or concept, of a “ring current” around Earth and its association with geomagnetic storms began in the early days of the twentieth century. -
<> CRONOLOGIA DE LOS SATÉLITES ARTIFICIALES DE LA
1 SATELITES ARTIFICIALES. Capítulo 5º Subcap. 10 <> CRONOLOGIA DE LOS SATÉLITES ARTIFICIALES DE LA TIERRA. Esta es una relación cronológica de todos los lanzamientos de satélites artificiales de nuestro planeta, con independencia de su éxito o fracaso, tanto en el disparo como en órbita. Significa pues que muchos de ellos no han alcanzado el espacio y fueron destruidos. Se señala en primer lugar (a la izquierda) su nombre, seguido de la fecha del lanzamiento, el país al que pertenece el satélite (que puede ser otro distinto al que lo lanza) y el tipo de satélite; este último aspecto podría no corresponderse en exactitud dado que algunos son de finalidad múltiple. En los lanzamientos múltiples, cada satélite figura separado (salvo en los casos de fracaso, en que no llegan a separarse) pero naturalmente en la misma fecha y juntos. NO ESTÁN incluidos los llevados en vuelos tripulados, si bien se citan en el programa de satélites correspondiente y en el capítulo de “Cronología general de lanzamientos”. .SATÉLITE Fecha País Tipo SPUTNIK F1 15.05.1957 URSS Experimental o tecnológico SPUTNIK F2 21.08.1957 URSS Experimental o tecnológico SPUTNIK 01 04.10.1957 URSS Experimental o tecnológico SPUTNIK 02 03.11.1957 URSS Científico VANGUARD-1A 06.12.1957 USA Experimental o tecnológico EXPLORER 01 31.01.1958 USA Científico VANGUARD-1B 05.02.1958 USA Experimental o tecnológico EXPLORER 02 05.03.1958 USA Científico VANGUARD-1 17.03.1958 USA Experimental o tecnológico EXPLORER 03 26.03.1958 USA Científico SPUTNIK D1 27.04.1958 URSS Geodésico VANGUARD-2A