COMSAT Technical Review

Total Page:16

File Type:pdf, Size:1020Kb

COMSAT Technical Review COMSAT Technical Review Volume 17 Number 1, Spring 1987 Advisory Board Joseph V. Charyk COMSAT TECHNICAL REVIEW John V. Evans Spring 1987 Editorial Board Geoffrey Hyde, Chairman Volume 17 Number 1 , Richard A. Arndt Ali E. Atia S. Joseph Campanella I DESIGN AND MODELING OF A GaAs MONOI.I'THIC 2- TO 6-GHz Dattakumar M. Chitre R. K. Gupta , .1. H. Reynolds, Russell J. Fang FEEDBACK AMPLIFIER Howard W. Flieger M. C. Fu , AND T. Heikkila Melvyn Grossman 23 A 120-Mbit/s TDMA QPSK MODEM FOR ON-BOARD APPLICATIONS Ivor N. Knight , AND F. T. Assal Larry C. Palmer R. G. Egri , K. Karimullab Edward E. Reinhart 55 AN ADAPTIVE EQUALIZER FOR 120-Mblt/s QPSK TRANSMISSION David V. Rogers Hans J. Weiss J. M. Kappes Albert E. Williams 87 MODULATION SELECTION FOR ILL MOBILE SATELI,FI'F EXPERIMENT Pier L. Bargellini, Editor Emeritus (MSAT-X) K. M. Mackenthun Editorial Staff MANAGING EDITOR Margaret B. Jacocks 105 HURWrrZ STABII .II'Y ANALYSIS OF AN ADPCM SYSTEM TECHNICAL EDITORS S. Dimolitsas AND U. Bhaskar Barbara J. Wassell Diane Haugen APPROXIMATIONS FOR THE RAISED COSINE FILTER PRODUCTION 127 POLE-ZERO J. J. Poklemba Barbara J. Wassell FAMILY Louis P. Stephens, Jr. 159 A SIMULATION STUDY OF RAIN ATTENUATION AND DIVERSITY EFFECTS CIRCULATION LINKS J. Mass Shirley H. Taylor ON SATELLITE COMSAT TECHNICAL REVIEW is published twice a year by 189 PROGRAMMABL E CONVOLUTIONAL ENCODER AND THRESHOLD Communications Satellite Corporation (COMSAT). Subscriptions, DECODER J. S. Snyder which include the two issues published within a calendar year, are: one year, $15 U.S.; two years, $25; three years, $35; 201 CTR NOTE : GEOSTATIONARY SATELLITE LOG FOR YEAR END 1986 single copies, $10; article reprints, $2.50. Overseas air mail C. H. Schmitt delivery is available at an additional cost of $18 per year. Make checks payable to COMSAT and address to Records Department, 267 TRANSLATIONS OF ABSTRACTS Communications Satellite Corporation, 22300 Comsat Drive, FRENCH 267 SPANISH 272 Clarksburg, MD 20871-9475, U.S.A. ISSN 0095-9669 277 AUTHOR INDEX, CTR 1986 COMMUNICATIONS SATELLITE CORPORATION 1987 COMSAT IS AIRADE MARK AND SERVICE MARK 279 LNDEX OF 1986 PUBLICATIONS BY COMSAT AUTHORS 01 HIE COMMUNICATIONS SATELLITE CORPORATION 111 Index: amplifiers, integrated circuits, ion implantation, MMICs, models, transistors Design and modeling of a GaAs monolithic 2- to 6-GHz feedback amplifier R. K. GUPTA, J. H. REYNOLDS, M. C. Fu, AND T. HtiKKILA (Manuscript receives December 3, 1986) Abstract The design, fabrication, and performance of a monolithic 2- to 6-GHz feedback amplifier module are described, with particular emphasis on the modeling approaches used during the design and fabrication phases. The amplifier design is based on GaAs field-effect transistor (rET) equivalent circuit parameters derived from known ion implantation profile, peak doping density, and device geometries. Measured parametric data obtained from test patterns arc used to monitor and control the fabrication process. Both measured and modeled DC and Rr parameters of the FEi, as well as amplifier performance results, are presented for two process wafers. Agreement between the measured and modeled gain of the feedback amplifier was within I dB over a broad I- to I1-GHz frequency band. Introduction The use of GaAs monolithic microwave integrated circuits (MMles) in communications systems holds great promise for enhancing system reliability while reducing mass, volume, and cost [11,[2]. However, the design and fabrication cycle for MM1c modules is relatively long and expensive compared to that of conventional hybrid circuits. In order to reduce development costs and enhance the probability of success in a single fabrication itineration, a thorough understanding of field-effect transistor (FET) models, from basic 1 GaAs MONOLITIBC 2- TO 6-GRZ FEEDBACK AMPLIFIER 3 2 COMSAT TECHNICAL REVIEW VOLUME 17 NUMBER 1, SPRING 1987 device physics through the fabrication process, design methods, and circuit CIRCUIT PERFORMANCE modeling, is required. REQUIREMENTS This paper presents the design, fabrication, and performance of an MMIC 2- to 6-GHz feedback amplifier module developed at COMSAT Laboratories. IMPLANT PROFILE / DEVICE SELECTION The design strategies and modeling approaches used during various MMIC MATERIAL DATA (CHANNEL GEOMETRIES) development phases are discussed. A PET equivalent circuit was first derived for a known ion implant profile, peak doping density, gate recess depth, and DEVICE RF EQUIVALENT DC CHARACTERISTICS CIRCUIT other fabrication parameters. The amplifier was then designed with maximum tolerance to process variations and with simple on-chip tuning to adjust for SELECTION OF the most sensitive parameters. The modeling process described here is useful MATCHING NETWORKS for selecting optimum FET geometries, designing the circuit for desired performance, and defining target values for critical process parameters and CAD DESIGN / MODELING adjusting these values during fabrication. In addition, accurate modeling of device Dc current and transfer characteristics allows a priori selection of device operating conditions for self-bias operation. SENSITIVITY ANALYSIS General design considerations The design of broadband feedback amplifiers requires LET devices with SATISFIES large transconductance [3]-[6]. This can be achieved by increasing the device FABRICATION TOLERANCES width and carrier concentration and decreasing the gate length. Larger device width also results in larger Dc power dissipation and larger gate-to-source capacitance, Cgf, which tend to degrade the open-loop gain at higher frequencies. Therefore, FETs with smaller gate lengths and a higher trans- CIRCUIT LAYOUT AND MASK MAKING conductance (gm)-to-Cgs ratio are desirable. Based on these considerations, a FET with a nominal gate length of 0.5 (or 0.6) µm and width of 300 [um was selected for this design. This FET geometry was consistent with other WAFER PROCESSING circuits on the same mask set, which included a low-noise amplifier ]7], a dual-gate FET switch with a level translator, and an amplifier with passive IN-LINE PARAMETRIC TESTS FET switching at its input and output. PROCESS To increase the yield, the MMIC design must be tolerant to fabrication ADJUSTMENTS parameter variations associated with process uncertainties. Therefore, a major COMPLETION OF FRONT-SIDE PROCESSING portion of the design effort involved developing accurate models for the active devices and the matching components, and establishing their sensitivity WAFER-LEVEL PROBING, to process variations. Figure 1 is a flow-chart of a typical MMIC design cycle. THINNING, DICING The design begins with device selection for desired electrical performance, and includes device modeling, design of matching networks, sensitivity analysis for acceptable performance, circuit layout, and mask-making. Circuit fabrication consists of processing the various mask layers, in-line parametric testing, fabrication adjustments, DC probing, thinning, and dicing. Because of the time consumed by each mask fabrication and processing cycle, it is Figure 1. Flowchart of the MMIC Design, Modeling, and Fabrication essential that a design be relatively insensitive to fabrication tolerances. Cycle 4 COMSAT TECHNICAL REVIEW VOLUME 17 NUMBER 1, SPRING 1987 GaAs MONOLITHIC 2- TO 6-GHZ FEEDBACK AMPLIFIER 5 FET modeling A number of models have been used at COMSAT Laboratories for the dP design of FETs and circuits [8],[9]. The FET model described here is based on device physics , with many refinements derived from measurements of a prototype device. For this design , the target Gaussian profile shown in Figure 2a was used with the following profile parameters: • Peak carrier density, He 2.7 x 1017 cm3 • Peak location , d„ 0.11 µm • Standard deviation , BE 0.065 p.m A recess depth up to the peak of the profile (0.11 µm), as shown in Figure 2b, results in a pinchoff voltage of approximately - 1.5 V and makes the De and RE device characteristics relatively insensitive to profile parameters. This profile information and measurements on the prototype device were as IJ do used to obtain the device equivalent circuit shown in Figure 3. Most of the 0 01 0.2 0.3 04 0.5 intrinsic FET elements, including junction capacitance, input resistance, and DISTANCE FROM ORIGINAL SURFACE (pm) device transconductance, were computed from the basic device physics. (a) Original Profile Output resistance, parasitic capacitances, and resistances were obtained from device geometries and measurements. 1018 I I I Junction capacitance, C, is modeled as the capacitance of the velocity- n„ ,P saturated region under the gate. Geometric inter-electrode capacitance caused by electrostatic coupling between the gate, source, and drain electrodes was computed as described by Pucel et al. [10]. Gate-to-N' and N'-to-N' (rather than gate-to-ohmic and ohmic-to-ohmic) gap dimensions were used. The N- 1017 material is sufficiently conductive to maintain an equi-potential surface over the short distances involved. A sidewall capacitance, which accounts for the extension of the depletion region toward the source, must be added to the gate-to-source fringing capacitance. The junction sidewall capacitance com- puted by the model is 0.04 pF and is included in the Cg of the device 1016 equivalent circuit. Input resistance, R;., represents a charging resistance corresponding to the gate-to-source capacitance. It is usually derived from an electron transit time, T, using resistance-capacitance (RC) time-constant relation as I do 1015 '{ I 0 0.1 0.2 0.3 0.4 R;,, = TICg, (I ) DISTANCE FROM ETCHED SURFACE (pm) The transit time is defined by (b) Profile After Recess Etch Figure 2. Gaussian ]on Implantation Profiles for the MMIC T=L,IV,. Feedback Amplifier GaAs MONOLITHIC 2- To 6-GHL FEEDBACK AMPLIFIER 7 6 COMSAT TECHNICAL REVIEW VOLUME 17 NUMBER 1, SPRING 1987 where V is the saturated velocity and L, is an empirically determined transit length. In the model, 16 = 1.2 X 107 cm/s and L, = 0.7 µm (geometric 0 gate length) were used. Transconductance, g,, is computed from basic device physics and is dependent on carrier profile, saturation velocity, and gate width.
Recommended publications
  • Satellite Systems
    Chapter 18 REST-OF-WORLD (ROW) SATELLITE SYSTEMS For the longest time, space exploration was an exclusive club comprised of only two members, the United States and the Former Soviet Union. That has now changed due to a number of factors, among the more dominant being economics, advanced and improved technologies and national imperatives. Today, the number of nations with space programs has risen to over 40 and will continue to grow as the costs of spacelift and technology continue to decrease. RUSSIAN SATELLITE SYSTEMS The satellite section of the Russian In the post-Soviet era, Russia contin- space program continues to be predomi- ues its efforts to improve both its military nantly government in character, with and commercial space capabilities. most satellites dedicated either to civil/ These enhancements encompass both military applications (such as communi- orbital assets and ground-based space cations and meteorology) or exclusive support facilities. Russia has done some military missions (such as reconnaissance restructuring of its operating principles and targeting). A large portion of the regarding space. While these efforts have Russian space program is kept running by attempted not to detract from space-based launch services, boosters and launch support to military missions, economic sites, paid for by foreign commercial issues and costs have lead to a lowering companies. of Russian space-based capabilities in The most obvious change in Russian both orbital assets and ground station space activity in recent years has been the capabilities. decrease in space launches and corre- The influence of Glasnost on Russia's sponding payloads. Many of these space programs has been significant, but launches are for foreign payloads, not public announcements regarding space Russian.
    [Show full text]
  • Descendants of Joseph Randolph
    Descendants of Joseph Randolph Generation 1 1. JOSEPH 1 RANDOLPH was born in 1750 in Spotsylvania County, VA. He died in 1810 in SC or GA. He married NANCY TURMAN . Notes for Joseph Randolph: Was a private in Revolutionary War. Joseph Randolph and Nancy Turman had the following child: 2. i. PEYTON SKIPWITH 2 RANDOLPH was born in 1792 in VA. He died on Jan 19, 1867. He married ELIZABETH FIELDS . She was born in 1796. She died on Apr 13, 1873. Generation 2 2. PEYTON SKIPWITH 2 RANDOLPH (Joseph 1) was born in 1792 in VA. He died on Jan 19, 1867. He married ELIZABETH FIELDS . She was born in 1796. She died on Apr 13, 1873. Notes for Peyton Skipwith Randolph: Died of pneumonia Notes for Elizabeth Fields: Died of pneumonia Peyton Skipwith Randolph and Elizabeth Fields had the following child: 3. i. PEYTON CALLAHAN 3 RANDOLPH was born on May 11, 1832. He died on Dec 03, 1893. He married Sarah Wallis Gilbert on Nov 15, 1869. She was born on Dec 17, 1839 in Saulsbury, TN. She died on Nov 02, 1931 in Mississippi. Generation 3 3. PEYTON CALLAHAN 3 RANDOLPH (Peyton Skipwith 2, Joseph 1) was born on May 11, 1832. He died on Dec 03, 1893. He married Sarah Wallis Gilbert on Nov 15, 1869. She was born on Dec 17, 1839 in Saulsbury, TN. She died on Nov 02, 1931 in Mississippi. Peyton Callahan Randolph and Sarah Wallis Gilbert had the following children: i. BENJAMIN FRANKLIN 4 RANDOLPH was born on Apr 07, 1870.
    [Show full text]
  • The Castor “Sputnik 50Th Anniversary Satellite Tracking Bonanza”
    CASTOR’SCASTOR’S “SPUTNIK“SPUTNIK 5050TH ANNIVERSARYANNIVERSARY SATELLITESATELLITE TRACKINGTRACKING BONANZA”BONANZA” 1957 2007 MICHAEL A. EARL CANADIAN SATELLITE TRACKING & ORBIT RESEARCH 4 OCTOBER 1957 SPUTNIK ORBITING THE EARTH THE FIRST-EVER SOVIET ARTIFICIAL SATELLITE OF THE EARTH 40 KOPECS – USSR MAIL USSR “SPUTNIK” STAMP HOWHOW MANYMANY SATELLITESSATELLITES AREARE ORBITINGORBITING USUS TODAY?TODAY? OVER 11,00011,000 INDIVIDUAL OBJECTS WE DEPEND ON SATELLITES EVERY SINGLE DAY WHATWHAT DOESDOES “SATELLITE“SATELLITE TRACKING”TRACKING” MEAN?MEAN? Detecting and observing artificial satellite(s) for some length(s) of time; Literally following it across the sky; Observing the object, relocating the detector to observe it again, etc.; Collecting data on the object as it is being detected and followed (tracking data); and Determining an orbit for the satellite using observations in order to detect it again on a future date. DO YOU THINK OF THIS WHEN YOU THINK OF “SATELLITE TRACKING”? WHATWHAT AREARE THETHE TWOTWO GREATESTGREATEST MODERNMODERN INNOVATIONSINNOVATIONS ININ ASTRONOMY?ASTRONOMY? THE GOTO TELESCOPE THE CCD CAMERA THETHE GOTOGOTO TELESCOPETELESCOPE ANDAND CCDCCD CAMERACAMERA The Goto Telescope allows the amateur astronomer to “point and click” onto objects of choice and slew the telescope to their locations in the sky; The Goto Telescope makes the astronomers’ lives easier by automatically knowing where the objects are located, i.e. no longer necessary to look up objects’ coordinates; The CCD Camera is much more sensitive than photographic film and can detect faint celestial objects much more effectively. Very large apertures are not as necessary. The CCD Camera has a linear response to light, therefore photometric measurements are much easier than with photographic film; The CCD Camera produces images that are already based on a grid (pixels).
    [Show full text]
  • Sts-51G Press Kit June 1985
    NATIONAL AERONAUTICS AND SPACE ADMINISTRATION SPACE SHUTTLE MISSION STS-51G PRESS KIT JUNE 1985 ARABSAT A; MORELOS A; TELSTAR 3-D; SPARTAN 1 Edited by Richard W. Orloff, 01/2001/Page 1 STS-5IG INSIGNIA S85-31266 -- The STS-51G insignia illustrates the advances in aviation technology in the United States within a relatively short span of the twentieth century. The flags of the French (Baudry) and Saudi Arabian (Al-Saud) payload specialists appear next to their name at the bottom of the insignia. The NASA insignia design for space shuttle flights is reserved for use by the astronauts and for other official use as the NASA Administrator may authorize. Public availability has been approved only in the form of illustrations by the various news media. When and if there is any change in this policy, which we do not anticipate, it will be publicly announced. PHOTO CREDIT: NASA or National Aeronautics and Space Administration. Edited by Richard W. Orloff, 01/2001/Page 2 RELEASE NO: 85-8 June 1985 CONTACTS Charles Redmond/Sarah Keegan Headquarters, Washington, DC (Phone: 202/453-8590) James Elliott Goddard Space Flight Center, Greenbelt, MD (Phone: 301/344-6256) David Alter Johnson Space Center, Houston, TX (Phone: 713/483-5111) Jim Ball Kennedy Space Center, FL (Phone: 305/867-2468) Ralph Jackson Dryden Flight Research Facility, Edwards, CA (Phone: 805/258-8381) Edited by Richard W. Orloff, 01/2001/Page 3 RELEASE NO: 85-83 June 1985 CONTENTS GENERAL RELEASE 5 51-G BRIEFING SCHEDULE 7 GENERAL INFORMATION 8 SHUTTLE MISSION 51-G -- QUICK LOOK FACTS
    [Show full text]
  • Satellite Data Communications Link Requirements for a Proposed Flight Simulation System
    Theses - Daytona Beach Dissertations and Theses 4-1994 Satellite Data Communications Link Requirements for a Proposed Flight Simulation System Gerald M. Kowalski Embry-Riddle Aeronautical University - Daytona Beach Follow this and additional works at: https://commons.erau.edu/db-theses Part of the Aviation Commons Scholarly Commons Citation Kowalski, Gerald M., "Satellite Data Communications Link Requirements for a Proposed Flight Simulation System" (1994). Theses - Daytona Beach. 266. https://commons.erau.edu/db-theses/266 This thesis is brought to you for free and open access by Embry-Riddle Aeronautical University – Daytona Beach at ERAU Scholarly Commons. It has been accepted for inclusion in the Theses - Daytona Beach collection by an authorized administrator of ERAU Scholarly Commons. For more information, please contact [email protected]. Gerald M. Kowalski A Thesis Submitted to the Office of Graduate Programs in Partial Fulfillment of the Requirements for the Degree of Master of Aeronautical Science Embry-Riddle Aeronautical University Daytona Beach, Florida April 1994 UMI Number: EP31963 INFORMATION TO USERS The quality of this reproduction is dependent upon the quality of the copy submitted. Broken or indistinct print, colored or poor quality illustrations and photographs, print bleed-through, substandard margins, and improper alignment can adversely affect reproduction. In the unlikely event that the author did not send a complete manuscript and there are missing pages, these will be noted. Also, if unauthorized copyright material had to be removed, a note will indicate the deletion. UMI® UMI Microform EP31963 Copyright 2011 by ProQuest LLC All rights reserved. This microform edition is protected against unauthorized copying under Title 17, United States Code.
    [Show full text]
  • Loral Space & Communications
    LORAL SPACE & COMMUNICATIONS LTD FORM 10-K (Annual Report) Filed 3/31/1997 For Period Ending 12/31/1996 Address 600 THIRD AVE C/O LORAL SPACECOM CORP NEW YORK, New York 10016 Telephone 212-697-1105 CIK 0001006269 Industry Electronic Instr. & Controls Sector Technology Fiscal Year 12/31 SECURITIES AND EXCHANGE COMMISSION WASHINGTON, D.C. 20549 FORM 10-K TRANSITION REPORT PURSUANT TO SECTION 13 OR 15(d) OF THE SECURITIES EXCHANGE ACT OF 1934 FOR THE TRANSITION PERIOD FROM APRIL 1, 1996 TO DECEMBER 31, 1996 Commission file number 1-14180 LORAL SPACE & COMMUNICATIONS LTD. 600 Third Avenue New York, New York 10016 Telephone: (212) 697-1105 Jurisdiction of incorporation: Bermuda IRS identification number: 13-3867424 Securities registered pursuant to Section 12(b) of the Act: NAME OF EACH EXCHANGE TITLE OF EACH CLASS ON WHICH REGISTERED - ------------------------------------------------------------------ ------------------------ Common Stock, $.01 par value...................................... New York Stock Exchange The registrant has filed all reports required to be filed by Section 13 or 15(d) of the Securities Exchange Act of 1934 during the preceding 12 months or such shorter period as the registrant was required to file such reports and has been subject to such filing requirements for the past 90 days. Disclosure of delinquent filers pursuant to Item 405 of Regulation S-K is contained in the registrant's definitive proxy statement incorporated by reference in Part III of this Form 10-K. At February 28, 1997, 191,092,308 common shares were outstanding, and the aggregate market value of such shares (based upon the closing price on the New York Stock Exchange) held by non-affiliates of the registrant was approximately $3 billion.
    [Show full text]
  • FCC-21-49A1.Pdf
    Federal Communications Commission FCC 21-49 Before the Federal Communications Commission Washington, DC 20554 In the Matter of ) ) Assessment and Collection of Regulatory Fees for ) MD Docket No. 21-190 Fiscal Year 2021 ) ) Assessment and Collection of Regulatory Fees for MD Docket No. 20-105 Fiscal Year 2020 REPORT AND ORDER AND NOTICE OF PROPOSED RULEMAKING Adopted: May 3, 2021 Released: May 4, 2021 By the Commission: Comment Date: June 3, 2021 Reply Comment Date: June 18, 2021 Table of Contents Heading Paragraph # I. INTRODUCTION...................................................................................................................................1 II. BACKGROUND.....................................................................................................................................3 III. REPORT AND ORDER – NEW REGULATORY FEE CATEGORIES FOR CERTAIN NGSO SPACE STATIONS ....................................................................................................................6 IV. NOTICE OF PROPOSED RULEMAKING .........................................................................................21 A. Methodology for Allocating FTEs..................................................................................................21 B. Calculating Regulatory Fees for Commercial Mobile Radio Services...........................................24 C. Direct Broadcast Satellite Regulatory Fees ....................................................................................30 D. Television Broadcaster Issues.........................................................................................................32
    [Show full text]
  • AVAILABLE from Hearing Before the Committee on Science and The
    DOCUMENT RESUME ED 392 400 IR 017 686 TITLE Educational Technology in the 21st Century. Joint Hearing before the Committee on Science and the Committee on Economic and Educational Opportunities. House of Representatives, One Hundred Fourth Congress, First Session. INSTITUTION Congress of the U.S., Washington, DC. House Committee on Economic and Educational Opportunities.; Congress of the U.S., Washington, D.C. House Committee on Science and Technology. REPORT NO ISBN-0-16-052181-5 PUB DATE 12 Oct 95 NOTE 365p.; Serial No. 104-37. Contains photographs which may not reproduce clearly. AVAILABLE FROMU.S. Government Printing Office, Superintendent of Documents, Congressional Sales Office, Washington, DC 20402. PUB TYPE Legal/Legislative/Regulatory Materibas (090) EDRS PRICE MF01/PC15 Plus Postage. DESCRIPTORS Computer Networks; *Computer Uses in Education; *Costs; *Educational Technology; Elementary Secondary Education; Expenditures; Futures (of Society); Hearings; Instructional Materials; *Technological Advancement IDENTIFIERS *Affordability; Congress 104th; *Future Learning; Grant Recipients ABSTRACT This document presents witness testimony and supplemental materials from a Congressional hearing addressing the potential as well as the affordability of educational technology and the classroom of the future, where computers and computer networks will increasingly aid teachers and facilitate learning. Those presenting prepared statements are Congressman George E. Brown, Jr., Congressman William Clay, Congressman Robert S. Walker, Congresswoman Lynn C. Woolsey, Congresswoman Constance A. Morella, and Congressman Randy 'Duke" Cunningham. Testimony is included from:(1) Seymour Papert, Massachusetts Institute of Technology; (2) Alan C. Kay, Apple Computer:(3) Chris Dede, George Mason University; (4) David E. Shaw, D. E. Shaw & Company;(5) Ed McCracken, Silicon Graphics;(6) Pat Wright, TCI Educational Technologies, Inc.;(7) Robert W.
    [Show full text]
  • TECHNOLD Official Trade Journal of the Society of Cable Television Engineers I
    COMMUNICATIONS TECHNOLD Official trade journal of the Society of Cable Television Engineers I ..._/ • ,.',,_ ___.,-.".-' -_',.,-''' -_-',,,e0K.:- _ _72 ,-- •••••••,..„ Handling the problems of lightning and power Wrapping up a successful Tec Expo August 1988 /tba Only one manufacturer's headend' e gg, equipment is reliable enough 1Ne/ ,br)a _ 4:0 ese) Ni,;:•fo .44 In addition to the standard Nexus 2Year is Warranty Extension to five years Limited NS arrranty, we are now pleased from the date of purchase applies to to offer an additional 3Year Warranty c„eNee 2 Year any Nexus headend equipment. Extension. This applies to ce` regardless of how long all Series 1, Series 5and you've owned it. Series 100 headend products. Of" Nexus will provide this For further information on valuable 3Year Warranty esee the Nexus Five Year Warranty si ts` Extension after you complete a earVVarranl, program, please call, write or market and application questionnaire. check the reader service number below. NEXUS - Built to Last. TEL: (206) 644-2371 OR WRITE: NEXUS ENGINEERING CORP. BELLEVUE. WA. 7000 LOUGHEED HWY. ENGINEERING CORR BURNABY, B.C.. V5A 4K4 (604) 420-5322 PERFORMANCE BURNABY, B.C. FAX: (604) 420-5941 YOU CAN - V>. CE. Reader Service Number 2. ,t11. 11k NO DROPOUTS Now that Trilogy has acomplete line shopping in all installations. of foam drop cables, you don't have to go Take it all the way in with Trilogy elsewhere to move inside after your MC and go forward with confidence with trunk and feeders are in place. the most rigorous quality control found in And you get the savings of one-stop the industry.
    [Show full text]
  • 7"-__F/,' "T C/7, E) Report to the NATIONAL AERONAUTICS AND
    NASA-CR-194177 /_- 7"-__F/,'_"t C/7, E) Report To The NATIONAL AERONAUTICS AND SPACE ADMINISTRATION - AMES RESEARCH CENTER - SEMIANNUAL STATUS REPORT #5 for GRANT NAG 2-700 SEARCH FOR EXTRATERRESTRIAL INTELLIGENCE/ HIGH RESOLUTION MICROWAVE SURVEY TEAM MEMBER Paul G. Steffes, Principal Investigator Report Period: March I, 1993 through August 31, 1993 Submitted by Professor Paul G. Steffes School of Electrical Engineering Georgia Institute of Technology Atlanta, Georgia 30332-0250 (404 894-3128) (NASA-CR-194177) SEARCH FOR N94-13086 EXTRATERRESTRIAL INTELLIGENCE/HIGH RESOLUTION MICROWAVE SURVEY TEAM MEMBER Semiannuel Status Report No. Unclas 5, 1 Mar. - 31 Aug. 1993 (Georgia Inst. of Tech.) 61 p G3155 0185928 TABLE OF CONTENTS Io INTRODUCTION AND SUMMARY II. DEVELOPMENT OF A DATA BASE OF SPACEBORNE TRANSMITTERS III. OBSERVATIONAL STUDIES IV. CONCLUSION V. REFERENCES Vl. APPENDICES 1. INTRODUCTION AND SUNiARY This semiannual status report describes activities conducted by the Principal Investigator during the first half of this third year of the NASA High Resolution Microwave Survey (HRMS) Investigator Working Group (IWG). As a (HRMS) Team Member with primary interest in the Sky Survey activity, this investigator attended IWG meetings at NASA/Ames and U.C. - Santa Cruz in April and August 1992, and has traveled independently to NRAO/KittPeak, Arizona (April Igg3) and Woodbury, Georgia (July 1993). During the July 1993 visit to the Georgia Tech Research Corporation/Woodbury Research Facility, an experiment was conducted to study the effects of interference from C-band (3.7 - 4.2 GHz) geostationary spacecraft on the Sky Survey operation in that band. At the first IWG meeting in April of this year, results of a SETI observation conducted at the 203 GHz positronium hyperfine resonance using the NRAO facility at Kitt Peak, AZ, were presented, as well as updates on the development of the spaceborne RFI data bases developed for the project.
    [Show full text]
  • CONGRESS of the INTERNATIONAL ASTRONAUTICAL FEDERATION BUDAPEST HUNGARY 10-15 OCTOBER 1983 M M XXXIV CONGRESS of the INTERNATIONAL ASTRONAUTICAL FEDERATION
    INIS-jnf—8969 BUDAPLCi <*» CONGRESS OF THE INTERNATIONAL ASTRONAUTICAL FEDERATION BUDAPEST HUNGARY 10-15 OCTOBER 1983 m m XXXIV CONGRESS OF THE INTERNATIONAL ASTRONAUTICAL FEDERATION ABSTRACTS OF PAPERS BUDAPEST, HUMGABr Oct. 10-15, FOREWORD Abstracts included in this book art ordered according to the IAF nuuber assigned to each paper eooepted for presentation at XZZI? IAP Congress. Experience hae shown that the chosen arrangement is the nost conrenient one and allows the easiest access to the abstraots. The IA? paper nuBber can be found in the Final Programe of the Congress under: - the Technical Session,wbere the paper is presented - the author's name, listed at the end of the Programe. The Abstracts of the Student Conference and of Space Law Colloquium are at the end of this book. Abstracts of papers arriTed later than August 1st are not included in thie collection. ftingarian Astronautieal Society - 2 - IAr-83~O1 EXOSAT/DELTA - DEMONSTRATED SHORT-TERM BACKUP LAUIfCHER CAPABILITY THROUGH INTERNATIONAL COOPERATION by J. K. Oanoung, Manager, Spacecraft Integration, Delta Program McDonnell Douglas Astronautics Company G. Altnann, EXOSAT Project Manager, European Space Agency P. Eaton, Chief, Expendable Launch Vehicle Programs National Aeronautics and Space Administration J. D. Kraft, Delta Mission Analysis and Integration Manager, National Aeronautics and Space Administration ABSTRACT An important exploration of eosnie x-ray sources currently under wey Wan made possible by a unique example of international cooperation. The EXOSAT spacecraft, designed, developed, qualified, and prepared for launch by the European Space Agency (ESA), was successfully launched by the National Aeronautics and Space Administration (NASA) Delta launch vehicle in May 1983* EXOSAT was originally scheduled for launch on the European Ariane rocket, but due to unforeseen schedule realignments, ESA, in cooperation with NASA, selected the Delta for this mission in February 1983.
    [Show full text]
  • International Cooperation and Competition in Civilian Space Activities
    International Cooperation and Competition in Civilian Space Activities June 1985 NTIS order #PB87-136842 Recommended Citation: International Cooperation and Competition in Civilian Space Activities (Washington, DC: U.S. Congress, Office of Technology Assessment, OTA-ISC-239, July 1985). Library of Congress Catalog Card Number 84-601087 For sale by the Superintendent of Documents U.S. Government Printing Office, Washington, DC 20402 Foreword The nature of global space activities has changed radically over the last decade. No longer are the United States and the Soviet Union the only countries capable of placing satellites into Earth orbit or sending interplanetary probes into deep space. Europe and Japan now have substantial space programs and have developed commercially competitive space systems. Several newly industrialized countries are well along in building their own space programs. In addition, the U.S. private sector has recently expanded its interest and investment in space technology. As this report makes clear, these changes have strong policy implications for the U.S. Government space program and for the U.S. private sector. This report presents the major findings of an assessment requested by the House Committee on Science and Technology and the Joint Economic Committee, on inter- national cooperation and competition in civilian space activities. The United States still enjoys a strong competitive position in most space technologies and in space science. There continues to be broad support for a long-term public commitment to civilian space activities. But precisely because of our achievements—and those of other space-far- ing nations—the number of opportunities (and associated costs) that lie before us re- quire a thoughtful articulation of space goals and objectives.
    [Show full text]