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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 KSC Historical Report No. 1 (KHR-1, Revised 1979) Eastern Test Range (ETR) July 1980 Western Test Range (WTR) A Summary of Major NASA Launches October 1,1958 - December 31,1979 1 A (NASA-TI-81 106) ). SUIIIARY 01 IAJOR NASA N80- 28386 LAUIVICRXS, 1 OCTOBER 1958 - 31 JECEIBEB 1979 (NASA) 201 p HC AlO/BF A01 CSCL 22A TJocl as , THOR MERCURY DELTA MERCURY ATLAS ATLAS GEMINI TlTANIll-E SATURN SATURN ACOLLO DELTA REOSTONE ATLAS AGENA CENTAc ,- TITAN II CENTAUR I I8 SATURN V SKYACOLLO LA8 SPACE SHUTTLE FORE WORU With the publ ication of this edition, "A Slmary of Major NASA Launches" nw spans more than twenty-one years in the launch history of the Nationa: Aeroriautics and Space Administrat.~on, frorn October 1, 1958, through Decanber 31, 1979. The initial brief sumnary of NASA Atlantic Missile Range (AMR) launches was pre- pared in 1962 as a reference tool for internal use within the Launch Operations Center Historical Branch. Repeated requests for infor~natioriconcerning f4ASA launch activities warranted the presentation of this information in handy form for broeder distribution. The Summary now includes major NASA launches conducted under the direction of the John F. Kennedy Space Center (or its precursors) from the Eastern and Western Test Ranges. It does not include launches of non-mi 1itary, non-NASA spacecraft by the U.S. Air Force or launches of the small NASA Scout vehicle. This edition supersedes 811 previous issues of this Historical R~port. The rnateri a1 contai ned in this report was compi 1ed from several different sour'ces. Docunents consulted include: Operations Sumnaries, post-launch Flash ~lisht Reports, Final Field Reports, Mission Operations Reports (both pre-launch and post-launch), and Satellite Situation Repor&. Other major references were publications of the NASA Historical Office, such as: Aeronautics and Astronautics 1916-1960; Aeronautical and Astronautical E vents of 1961-1962 ; Aeronautics and Astronautics (yearly editions since f96T,mgs Pocket Statistics (published monthly). The writer is indebted to Mr. Marven R. Whipple, USAF ETR Historian, now retired, for providing data not otherwise available, and to Mr. William A. Lockyer, who prepared the previous edition of this report. Ms. Donna A. Clement, Mr. Joseph L. Green, and Mr. Hubert E. Griggs, McGregor-Werner Information Services Unit, provided valuable editorial assistance. The report is divided into projects within broad mission categories. Individual launches are listed In chronological order vif5in the categories. Mission results have been categorized as: successful (S); unsuccessful (U) ; or, pdrtially successful (P). A successful launch, fol lowed by a spacecraft fai lure, is designated (P). These are arbitrary classifications, made after a comparison of objectives and actual resul ts. A similar document, prepared in chart form, is available up011 request. Comnents, criticismns, and suggest ions for the ilnprove~nentof this publ ication are sol icited. Correspondence should be addressed to KSC Historical Services (SI-SRV- 1) , John F. Kennedy Space Center, tIASA, Kennedy Space Center, Florida 32899. Francis E. Jarrett KX Historian ..... ..... ..... ..... .....a*.*. ..... ..... ..... ..... ......a*.. .......me. ..... ..... ......a.m. ..... ..... ..... ..... ..... ..... ..... ..... mn. om a*. .. :zme :... : : il...... na.....J ... z %%: :H =I- .W z 32 . .I- W JY. L uu. .m.- -1JCYLIC 9 eor -00 0 WWW* WWWW a Lza>% OO=rQ?L 2 --u==) naemJ or I 3 A ............. ...0.. ....... ... ............... ... ....... ... ....... ... ....... ... ....... ... ....... ... ....... h.. ... :::i#::...... ... 0.0 ... ....... C.. .. ... ..........Is.. ... ....V). ... ::::%:: ... ....u.. ... n... .. V)...Wr. ... .C ... Oh. =:..n.. n***d*. .V) . C...-l.. .O u. OW" . .W 0. .+V) . 0- :s W .u 3 : c, :d, :*- : -w. -I .O .A V)t A .L .UW 0'- .CC WA :U .zn -u-ad : i#ii CV) m-Y) .OC ess ZUO :zgi : ZzS z3z AUA CkJY *L-J.> :. >-au :ws. ewu- CYCU .A- sOe wmr .u(1 An V) 0 .LO mcnn e0-l 2si OOC .uO * nzw CU .CP: CWC 0-a *ua . Z U w u maw : -mum a-1n .WC Qca uuo .nu az .or OZZ LOV) . I%T -+aL-0 .** . CWS <u : Lac+ :z%*LZ 2-rwua -00 -0 Zk!O .UUC. mow .*be 2ss >meem +z 51m03*C-o w * a: W0OCPOV)V)L' OQW AOCQZOOC 00- w-r-WWW * wwe Cb-Zaa3E m '3aJ TABLE OF COHTENTS (Continued) PAGE MANNED SPACE FLIGHT MERCURY GEMINI APOLLO MSFN TRAINING SATELLITESa~aaaaaaa*~aaa~aaaaaa*a~a~~~aaaaaaaaaaaaaaaaaaaaaaaaaaaV-12 SUBORBITAL~~~~~~~*~~~~~~~~~~~~a~~~*~~~~~aaaV-14 EARTH ORBITALaaaaaaa~a~aaaaa~~~aaaaaaaa~aaaa~aaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaV-16 LUNAR 0RBITAL~a.a.a~~aaaaaaaaaaaaa~aaaaaa~a~aaa~aaaaaaaaaaaaaaaaaaaaaaaaaaaoV-23 LUNAR LANDINGa~aa.a.a*aaaaa****aa~*acaaa~aaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaV-25 SKY LAB APOLLO-SOY UZ TEST PROJECT APPENDICES A: SUMMARY OF LAUNCHES PRIOR TO OCTOBER 1958 IN SPACE PROJECTS LATER TRANSFERRED TO MSA VANGUARD**aa*aa*...aaaaa~aca~~aaaa~aaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaaA02 EXPLORERaaaaa*a*aaaaaaaaa~aaaaaaa~aaa~a~aaaaaaaaaaaaaaa*aaaaaaaaaaa*aaaaaaaaaaaaA-6 PIONEERa*.a.aao.aa*aa**aaaaaa*aeaaa~*aaaa a.aaaaaa.aaaa*aaaaa*aaaaaa*aa*aa~aa*aaaaaa*aaa A09 8: CHRONOLOGICAL IfiDEX OF LAUNCHES~~.a*.*.a~aaaaa*a~~~a~aa*aaa*aaaaa**a*a**a*aaaaaaaaaaaaa8-1 C: ALPHABETICAL INDEX OF LAUNCHESaa~~aa.....~..a~~aaa*oaaaaa**~aaaaaaaaaaaaaaaaC-1 a, 9 9 5?8 rC) c-* 4s %a- -- m SF+@ r a* a @4Q)O'II -"Ps *r. U- OS'SaO~*~Z rw- &e t! g$ s""> 4 C'rU' 4zms= L ow- Y) -@- as VL su- -0)OY)~gl*gte taB=I6 vDz'E@ 2s9 '3 z L@C na~umo m* urL I ameg ~NS0 04 n uuwB 0 - - I P (nhr 0 cn COW Po@mw 0)dOIOU 3-n @ '~~'5 mu, 0) c u, 0)m 1 ce, a, Et &rI wgscll$Zi L--EWY) 0- u,rcn- C worn% --BOcrPLE 0) ULO P"P g x zc cz 8=5 cll r,c.aiiCU 3 -2%C & ce, cc C 84a cll c,s - - cn U 0) i$ase* 0 C.- 0)-a 0 C L -0 p 2 g;: ZgQ-c arc*, \ EoIma esw-' E WV) I L C a 8'a*, he9- -s C - r mC .ru3- B C L cd C 8 a 9-t 0 .r .C 0 UP- .r .* C L C Q)- m-3 x .r au a 0- IC 0 cn .C) 5 o 9.C J cC) 5% (U Pa, x n mu, A a a hV) aual 0- Or- E = P Fi cn -0 aC, al 0 Eu, =5= Y maQ)L~ o C a!at C, 9.0 cn a .c A h u LL 7 -w rJ ZS urn 4 urn 'Qrn ,a 4 2.2 or: C,dv 0 1 or: 3s Flal aQ) 5s 53 > 3- m= 3-59 3- PHYSICS AND ASTRONOMY (continued) Mission Launch Launch NASA Sitc/ Name Date/Time Vehicle -Code -Pad Renarks/Resul ts Explorer 12 15 Aug 61 Delta S-3 ETR 37.64-kg (83-lb) spacecraft designed to provide 2221 EST DM-19 17A data on magnetic fields, energetic partfcles, and (Del ta-6) solar wind. Data received from all utperiaents; transmitted until 6 December 1961; re-entered in Septenber 1963. (S) Explorer 14 2 Oct 62 Delta S-3a ETR 36.28-kg (80-1 b) spacecraft injected into highly I 1711 EST DSV-3A 170 elliptical orbit--98,476 x 280 km (61,190 x 974 I (Del ta-13) sm), inclination 33O, period 36.4 hours. Energetic particles experiment. Sti11 in orbit, but orbital elements no longer maintained. Data transmission continued until 10 August 1963. (S) Explorer 15 27 Oct 62 Delta S-3b ETR A 44.45-kg (98-lb) satellite to stu4y artificial 1815 EST DSV -3A 178 radiation belt. High spin rate, still in orbit, (Del ta-14) but orbital elements no longer maintained. (S) Explorer 17 2 Apr 63 Del ta S-6 ETR A 183.7-kg (405-lb) satellite studied density, 2100 EST DSV-3B 17A pressure, composition, and temperature of the (Del ta-17) Earth's upper atmosphere. Re-entered on 24 November 1966. (S) Explorer 18 26 Nov 63 Del ta IMP-A ETR Successful launching of an Interplanetary hi tor- 2130 EST DSV- X (S-74) 170 ing Probe; its mission was to measure the f~jor (Del ta-21) magnetic field phenomena in space, incfudijcg the interplanetary magnetic field, interactiws of the streaming solar plasma, and the qeomagnetic field, galactic and solar radiation. Rz-entered in Decelllber 1965. (S) \ we k-h Ecno Wrc -iD- PY rn-WV) -e- CU Q) I Sr- W UV (Om@ C-r @I- =Is FWQ) 'waJ acne A> no- PHYSICS AND ASTRONOMY (continued) Mission Launch Launch NASA Site/ Name .Date/Time Vehicle -C ode -Pad Remarks/Resul t s Explorer 31 28 Nov 65 Thor-Agena DME-A WTR Dual launch of 98.88-kg (218-lb) spacecraft with 2349 EST (Thrust- SLC-2E Alouette 2 (total pa: load 245 kg--541 lb). Com (2049 PST ) Augmented) plemented A1 ouette by taking measurements of iono- (Thor- spheric characteristics with a companion Agena-5) spacecraft as part of ISIS-X program. Sti11 in orbit ; sti11 transmitting. Orbital parameters are: 2,939 x 505 krn (1,826 x 314 sm), period 121 mins, inclination 79.s0. (S) E~plorer32 25 May 66 Dei ta AE-B ETR Atmosphere Explorer; the 224.5-kg 1495-lb) payload 0900 EST DSV-3C (S-6 a) 178 was desi gned to col 1ect temperat composition, (Del ta-38) density, and pressure data to perlnlt the study of the physics of the atmosphere on a global basis. Still in orbit--1,664 x 255 km (1,034 x 158 sm), period 104 mins, inclination 64.6'.
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    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
  • Fiscal Year 1973, and Are the EROS Program Also Supports the ERTS Data Proiected at Almost $1 Million for Fiscal Year 1974

    Fiscal Year 1973, and Are the EROS Program Also Supports the ERTS Data Proiected at Almost $1 Million for Fiscal Year 1974

    Aeronautics and Space Report of the President r973 Activities NOTE TO READERS: ALL PRINTED PAGES ARE INCLUDED, UNNUMBERED BLANK PAGES DURING SCANNING AND QUALITY CONTROL CHECK HAVE BEEN DELETED Aeronautics and Space Report of the President 1973 A c tivities National Aeronautics and Space Administration Washington, D.C. 20546 President’s Message of Transmittal To the Congress of the United States: the European Space Conference has agreed to con- struct a space laboratory-Spacelab-for use with the I am pleased to transmit this report on our Nation’s Shuttle. progress in aeronautics and space activities during Notable progress has also been made with the Soviet 1973. Union in preparing the Apollo-Soyuz Test Project This year has been particularly significant in that scheduled for 1975. We are continuing to cooperate many past efforts to apply the benefits of space tech- with other nations in space activities and sharing of nology and information to the solution of problems on scientific information. These efforts contribute to global Earth are now coming to fruition. Experimental data peace and prosperity. from the manned Skylab station and the unmanned While we stress the use of current technology to solve Earth Resources Technology Satellite are already being current problems, we are employing unmanned space- used operationally for resource discovery and manage- craft to stimulate further advances in technology and ment, environmental information, land use planning, to obtain knowledge that can aid us in solving future and other applications. problems. Pioneer 10 gave us our first closeup glimpse Communications satellites have become one of the of Jupiter and transmitted data which will enhance principal methods of international communication our knowledge of Jupiter, the solar system, and ulti- and are an important factor in meeting national de- mately our own planet.
  • Solar Parameters for Modeling Interplanetary Background

    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.