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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. -
Jacques Tiziou Space Collection
Jacques Tiziou Space Collection Isaac Middleton and Melissa A. N. Keiser 2019 National Air and Space Museum Archives 14390 Air & Space Museum Parkway Chantilly, VA 20151 [email protected] https://airandspace.si.edu/archives Table of Contents Collection Overview ........................................................................................................ 1 Administrative Information .............................................................................................. 1 Biographical / Historical.................................................................................................... 1 Scope and Contents........................................................................................................ 2 Arrangement..................................................................................................................... 2 Names and Subjects ...................................................................................................... 2 Container Listing ............................................................................................................. 4 Series : Files, (bulk 1960-2011)............................................................................... 4 Series : Photography, (bulk 1960-2011)................................................................. 25 Jacques Tiziou Space Collection NASM.2018.0078 Collection Overview Repository: National Air and Space Museum Archives Title: Jacques Tiziou Space Collection Identifier: NASM.2018.0078 Date: (bulk 1960s through -
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 -
1. State of the Magnetosphere
VOL. 78, NO. 16 3OURNAL OF GEOPHYSICAL RESEARCH 3UNE 1, 1973 SatelliteStudies of MagnetosphericSubstorms on August15, 1968 1. Stateof the Magnetosphere R. L. M CPHERRON Department o] Planetary and SpaceScience and Institute o] Geophysicsand Planetary Physics University o] California, Los Angeles,California 90024 The sequenceof eventsoccurring throughou.t the magnetosphereduring a substormhas not been precisely determined. This paper introduces a collection.of papers that attempts to establish this sequencefor two substormson August 15, 1968. Data from a wide variety of sourcesare used, the major emphasisbeing changesin the magnetic field. In this paper we use ground magnetograms to determine the onset times of two substorms that occurred while the Ogo 5 satellite was inbound on the midnight meridian through the cusp region of the geomagnetictail (the region of rapid changefrom taillike to dipolar field). We concludethat at least two worldwide substormexpansions were precededby growth phases.Probable begin- nings of these phaseswere at 0330 and 0640 UT. However, the onset of the former growth phase was partially obscuredby the effects of a preceding expansionphase around 0220 and a possible localized event in the auroral zone near 0320 UT. The onsets of the cor- respondingexpansion phases were 0430 and 0714 UT. Further support for these determina- tions is provided by data discussedin the subsequentnotes. The precise sequenceof events that occurs Ogo 5 in the near tail, and ATS I at syn- during a magnetosphericsubstorm has not been chronousorbit. Solar wind plasma parameters established.Among the reasons for this are were measured by Vela 4A. Magnetospheric lack of consistencyin the definition of sub- convection is inferred from a combination of storm onset and the wide variability of suc- plasmapauseobservations on Ogo 4 and 5 in cessivesubstorms. -
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. -
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. -
Desind Finding
NATIONAL AIR AND SPACE ARCHIVES Herbert Stephen Desind Collection Accession No. 1997-0014 NASM 9A00657 National Air and Space Museum Smithsonian Institution Washington, DC Brian D. Nicklas © Smithsonian Institution, 2003 NASM Archives Desind Collection 1997-0014 Herbert Stephen Desind Collection 109 Cubic Feet, 305 Boxes Biographical Note Herbert Stephen Desind was a Washington, DC area native born on January 15, 1945, raised in Silver Spring, Maryland and educated at the University of Maryland. He obtained his BA degree in Communications at Maryland in 1967, and began working in the local public schools as a science teacher. At the time of his death, in October 1992, he was a high school teacher and a freelance writer/lecturer on spaceflight. Desind also was an avid model rocketeer, specializing in using the Estes Cineroc, a model rocket with an 8mm movie camera mounted in the nose. To many members of the National Association of Rocketry (NAR), he was known as “Mr. Cineroc.” His extensive requests worldwide for information and photographs of rocketry programs even led to a visit from FBI agents who asked him about the nature of his activities. Mr. Desind used the collection to support his writings in NAR publications, and his building scale model rockets for NAR competitions. Desind also used the material in the classroom, and in promoting model rocket clubs to foster an interest in spaceflight among his students. Desind entered the NASA Teacher in Space program in 1985, but it is not clear how far along his submission rose in the selection process. He was not a semi-finalist, although he had a strong application. -
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.