Verification Test Plan
|
|
- Beatrix Fox
- 6 years ago
- Views:
Transcription
1 (Note: the configuration data provided in this test plan is subject to change.) Antenna Verification Testing and scheduling Tel: Cell phone: Fax: Antenna Diameter (meters) Latitude (deg) North Refer to: Max EIRP Capability (dw) SSOG 200, SSOG 210 Nominal TX Gain (di) Longitude (E) (deg) East 15 MAY 2001, REV 5 Nominal 3 d eamwidth (deg) Earth Station Support Azimuth Step Size (deg) Registration Elevation Step Size (deg) Fax: AZ angle to test satellite (deg) EL angle to test satellite (deg) Page 1 of 6 Test Information Tests to be Performed Test Dates 01 Mar 2001 Contact Name Gain Over Temperature Time(UTC) 12: Earth Station Name TX Isolation Contour Satellite deg Earth Station Under Test (EUT) TX Antenna Patterns/Gain Cuts Telephone Tracking and EIRP Stability FAX Transmit Gain (Carrier match) Refer to <RXUVFKHGXOHGWHVW HPA Stability (This test is not mandatory but recommended.) WLPHGDWHDQGWKH VSDFHFUDIWWKDWZLOO EHXVHGIRUWKHWHVW Antenna Information 6WHSVL]HLQIRUPDWLRQ XVHGIRUWKHLVRODWLRQ FRQWRXUWHVW 7KHWHVWVWKDW\RX DUHUHTXLUHGWR SHUIRUPDUHOLVWHG KHUH Available Spacecraft eacons Ku-and C and RHCP RHCP LINEAR APR RHCP RHCP (Horizontal) LINEAR LINEAR (Vertical) LINEAR LINEAR APR-1 (Vertical) NOTE: 3950 MHz beacon on the IS E satellite is phased at 45
2 Test Configuration Information RX Tests YHULILFDWLRQ Configuration WHVWV 1 Configuration 2 On request and CSM resources U/L D/L U/L D/L permitting, AVT can provide a test Frequency (MHz) Frequency (MHz) carrier during EUT test time for non Transponder Transponder mandatory receive tests. eam GLO/A GLO/A eam GLO/ GLO/ Polarization LHCP RHCP Polarization RHCP LHCP S/C Isolation (d) S/C Isolation (d) Transmit Gain Note: Transmit gain by carrier match method depends in part on the accuracy of the measurement of EUT feed flange power. This method will only be used when 7KLVFROXPQSURYLGHVJHQHUDO LQIRUPDWLRQUHOHYDQWWRDQWHQQD Transmit Gain EUT has no antenna drive mechanism. Transmit gain is normally measured as part of pattern cuts using pattern integration. If the EUT does not have a motor drive antenna then carrier match transmit gain will have to be performed. Page 2 of 6 7KHIUHTXHQF\EHDPFRYHUDJH DQGSRODUL]DWLRQWKDWZLOOEH XVHGIRU\RXUYHULILFDWLRQWHVW EIRP/Tracking Stability Note: EIRP/Tracking stability is mandatory for all antennas with tracking capability. It is not mandatory for EUT s without tracking capability. It is recommended that these EUT s monitor the HPA output into dummy load or to clear sky for a period of twelve hours. HPA output can be measured by a Strip chart recorder or manually recording the level at an interval of every 15 minutes. EUT will transmit a test carrier. AVT will benchmark the carrier downlink. AVT will then transmit a test carrier at the same level as the EUT. Refer to the SSOG 210 for details. EIRP/Tracking Stability Test To measure the EIRP and tracking stability of the EUT over a period of twelve hours. AVT will record the downlink EIRP and frequency of the EUT test carrier and associated beacon for a period of twelve hours. EUT will record weather conditions during the test and report any change in conditions which could adversely effect the test.
3 Page 3 of 6 G/T Procedure Direct Spectrum Analyzer STEP 1: Manually peak antenna Azimuth and Elevation axis on beam center of S/C beacon or carrier signal. The preferred more accurate me thod for G/T measurement is using a carrier versus a satellite beacon. In both cases the downlink EIRP must be measured by AVT. STEP 2: The polarization angle should be optimized if the feed is linearly polarized. STEP 3: Set Spectrum Analyzer parameters as follows Resolution bandwidth 1 khz Video andwidth 100 Hz Span 50 khz Amplitude/division 10 d Reference level - convenient value, for example -30 to 50dbm depending on the level of the carrier or beacon being measured. Adjust signal level towards the top gradicule of the screen. STEP 4: Do not change the above settings on the spectrum analyzer. Select Marker/Noise On (dm/hz). Record the level and plot the display again. Remove signal (cable) from the input to the spectrum analyzer and verify the noise floor of the instrument is less than sky noise by a margin of at least 8-10d. STEP 5: Select Marker normal (dm) and then Peak Search. Record the level. Plot or print the spectrum analyzer display. A digital photographic image of the screen is also acceptable. Digital photographs can be sent as a bitmap/ JPEG via to avt@intelsat.int STEP 6: Remove the uplink carrier if being radiated by AVT or antenna under test. Point antenna off the satellite at least 10 degrees to quiet (cold) sky in azimuth CW or CCW direction. STEP 7: Fax and /or the 3 plots made in steps 4,5,6 [(C+N), sky noise and spectrum analyzer noise floor plots] to AVT at (202) AVT staff will immediately perform calculation of G/T. Please annotate plots as to polarization, sky-noise and instrument noise floor.
4 Receive G/T Note 1: If measuring G/T by spectrum analyzer direct method using a spacecraft beacon, the beacon downlink EIRP must be measured by AVT at the time of G/T measurement. Verification Test Plan Page 4 of 6 Receive System Figure of Merit (G/T) (Direct Spectrum Analyzer.) This form must be completed and faxed to AVT ( ) following G/T measurement. To measure the ratio of receive gain of the earth station antenna to the total noise temperature of the earth station receive system. Using satellite or celestial source the EUT will acquire the test signal. Using a spectrum analyzer the EUT will record the peak of the test signal. EUT will then point off the source and measure the noise. Note 2: Standard A and C Test Time (UTC) antennas require that G/T be Test Date: measured using radio star method. Intelsat Earth Station Code: For other standard antenna G/T is Spectrum analyzer manufacturer: measured by spectrum analyzer Spectrum analyzer model number: direct method using either EUT longitude (see note 4) spacecraft beacon or an EUT latitude (see note 4) unmodulated test carrier radiated by AVT.,IWKHGLUHFWVSHFWUXP DQDO\]HUPHWKRGLVXVHG IRU*7WKHGDWDPXVW EHUHFRUGHGRQWKLVIRUP DQGID[HGWR$97DORQJ ZLWKWKHVSHFWUXP DQDO\]HUSORWV Note 3: Please fax carrier LHCP or Horizontal RHCP or Vertical and noise level plots with the Intelsat Spacecraft G/T information if available. Satellite Location (deg E) Test Frequency Note 4: If transportable, please Earth Station elevation angle (deg) provide the geographic coordinates of the EUT where Non-direct Reading Specan measurement was made. Carrier + Noise level (dm) Sky Noise level (dm or dm/hz) Note 5: Spectrum analyzer noise Spectrum analyzer noise floor (dm or dm/hz) floor reading should be measured Resolution andwidth with no input to instrument (cable Correction Factor (eg 0.75 or 1.2) removed) Spec is 8-10d below noise level measured with antenna pointed Direct Reading Spectrum Analyzer off spacecraft to quiet sky. C/No measured (d/hz)
5 Isolation Contour Test Page 5 of 6 Common Problems: 1. Isolation contour is not centered at position 1. EUT antenna must be accurately peaked at beam center before commencing the isolation contour. 2. Non compliant isolation results. The purpose of the Isolation Contour Test is to measure the crosspol performance of the EUT at the 0.5d and 1 d beamwidths of the antenna. The EUT will radiate an unmodulated carrier to the assigned spacecraft at sufficient level to provide the nominal downlink EIRP as provided by the test plan. The nominal downlink will typically be 15 dw for C and, and 25 dw for Ku-band. From Position 1 (beam center), the EUT will follow the offsets indicated below. AVT will measure copol and xpol downlink E.I.R.P. at each position in order to determine the transmit isolation. Ensure that shorting plates on any Un-used ports are removed and the port is correctly terminated. Position 5 Position 4 Position 3 All waveguide flanges and +EL / -AZ offset +EL / 0 AZ offset +EL / +AZ offset connectors should be secure and tight. Polarizer must be correctly aligned with spacecraft used for testing (K band feeds). Null adjustment will be performed at position 1 3. EUT does not have Angle Position 6 Position 1 Position 2 display 0 EL / -AZ offset No offsets 0 EL/+ AZ offset eam Center In this case AVT will instruct EUT to stop antenna movement as each position is reached. EUT must be able to move the antenna accurately in small increments. Position 7 Position 8 Position 9 -EL / -AZ offset -EL / 0 AZ offset -EL / +AZ offset
6 Transmit Antenna Patterns Page 6 of 6 A C UP RETRACT (RET) A C UP EXTEND (EXT)) A C RETRACT (RET) A C EXTEND (EXT) CW CW To demonstrate compliance with mandatory sidelobe pattern specification provided in the IESS document for the antenna standard under test. To measure the transmit gain of the antenna so that sidelobe and off axis emission requirements can be demonstrated. To provide additional data on cross polarization performance. Antenna patterns will be performed over +/- 12 degrees. AVT will provide secant corrections for elevation over azimuth mounts. To correct for non-linearity of jackscrew type antenna drive systems EUT must provide jackscrew dimensions in both azimuth and elevation. EUT will move the antenna to a point slightly greater than -12degrees to allow for startup errors due to antenna inertia. At AVT request, the EUT will move the antenna and provide a MARK at the start, beam center and stop points. Direction of Jackscrew for upward movement of antenna: EXT or RET Azimuth C = Meters Slew rate = deg/sec Azimuth CA = Meters Azimuth A = Meters Top view Direction of Jackscrew for clockwise movement of antenna: EXT or RET Elevation C = Meters Slew rate = deg/sec Elevation CA = Meters Elevation A = Meters Side view (/(9$7,21 %-$&.6&5(: -$&.6&5(: $02725,I\RXUDQWHQQDKDVD MDFNVFUHZ\RXPXVWPHDVXUH DQGUHFRUGMDFNVFUHZDQGVOHZ UDWHLQIRUPDWLRQSULRUWR DQWHQQDSDWWHUQWHVWLQJ &(/(9$7,21$;,6 %Ã-$&.6&5(:3,927 & $=,087+ $;,6 $ Ã-$&.6&5(:3('(67$/3,927 (/(9$7,21$;,6 09/06/2814A Ã)RUÃ(OHYDWLRQÃ3LYRWÃVHHÃ$]LPXWKÃSURMHFWLRQ
Earth-Stations. Performance Requirements
AMOS-Satellites System Earth-Stations Performance Requirements Version 4.33 August 2013 1 TABLE OF CONTENTS GENERAL INFORMATION... 3 1. GENERAL... 4 2. ANTENNA... 5 2.1. TRANSMIT SIDE-LOBES (MANDATORY)...
More informationSatellite Link Budget 6/10/5244-1
Satellite Link Budget 6/10/5244-1 Link Budgets This will provide an overview of the information that is required to perform a link budget and their impact on the Communication link Link Budget tool Has
More informationProject: 3.8M Series 1385 Ku-Band Rx/Tx System. General Dynamics SATCOM Technologies
Antenna Test Report Test No. 1761 Project: 3.8M Series 1385 Ku-Band Rx/Tx System. SATCOM Technologies East Maiden Antenna Test Facility 4488 Lawing Chapel Church Road Maiden, North Carolina 2865 828-428-1485
More informationRECOMMENDATION ITU-R S.1512
Rec. ITU-R S.151 1 RECOMMENDATION ITU-R S.151 Measurement procedure for determining non-geostationary satellite orbit satellite equivalent isotropically radiated power and antenna discrimination The ITU
More informationDifferent Elements in Receive Chain. Dish Parabola Feed LNBC RF Cable Divider Receiver
Art of Dish Tuning Indian Curry Little bit of Technical & More of Practical Layman Dialogue Mainly aimed for Grass-root level Dish Tuning Not a Conventional Kind of Lecture. More of Interactive Kind of
More informationITU/ITSO Workshop on Satellite Communications, AFRALTI, Nairobi Kenya, 8-12, August, Link Budget Analysis
ITU/ITSO Workshop on Satellite Communications, AFRALTI, Nairobi Kenya, 8-12, August, 2016 Link Budget Analysis Presenter: E. Kasule Musisi ITSO Consultant Email: kasule@datafundi.com Cell: +256 772 783
More informationFCC 47 CFR PART 15 SUBPART C INDUSTRY CANADA RSS-210 ISSUE 8 BLUETOOTH LOW ENERGY CERTIFICATION TEST REPORT FOR. 2.4GHz LE MODULE MODEL NUMBER: RN4020
FCC 47 CFR PART 15 SUBPART C INDUSTRY CANADA RSS-210 ISSUE 8 BLUETOOTH LOW ENERGY CERTIFICATION TEST REPORT FOR 2.4GHz LE MODULE MODEL NUMBER: RN4020 REPORT NUMBER: 14U17191-1 ISSUE DATE: MARCH 21, 2014
More informationParadigm. Connect100 Installation Guide
Paradigm GX Connect100 Installation Guide Paradigm GX Safe Use WARNING Radiation Hazard. Transmitter power levels are sufficient to cause blindness or other serious injury to body tissue. Do not power
More informationSIGFOX END- PRODUCT RADIATED TEST PLAN FOR SIGFOX READY TM CERTIFICATION
October 5 th 2017 SIGFOX END- PRODUCT RADIATED TEST PLAN FOR SIGFOX READY TM CERTIFICATION Public use Revision History Revision Number Date Author Change description 0.1 August 15 th, 2017 B.Ray Initial
More informationFLYAWAY SYSTEMS. communications
FLYAWAY SYSTEMS communications communications FLYAWAY Antenna Series The Temix Flyaway Antenna series is designed to answer to the hardest demands of reliable operations also in extreme environmental conditions
More informationRECOMMENDATION ITU-R SNG * Uniform technical standards (analogue) for satellite news gathering (SNG)
Rec. ITU-R SNG.722-1 1 RECOMMENDATION ITU-R SNG.722-1 * Uniform technical standards (analogue) for satellite news gathering (SNG) (1990-1992) The ITU Radiocommunication Assembly, considering a) that satellite
More informationEuropean Radiocommunications Committee (ERC) within the European Conference of Postal and Telecommunications Administrations (CEPT)
European Radiocommunications Committee (ERC) within the European Conference of Postal and Telecommunications Administrations (CEPT) ASSESSMENT OF INTERFERENCE FROM UNWANTED EMISSIONS OF NGSO MSS SATELLITE
More informationSECTION 2 BROADBAND RF CHARACTERISTICS. 2.1 Frequency bands
SECTION 2 BROADBAND RF CHARACTERISTICS 2.1 Frequency bands 2.1.1 Use of AMS(R)S bands Note.- Categories of messages, and their relative priorities within the aeronautical mobile (R) service, are given
More informationTest specification: Section (e)(1), Radiated emissions below 40 GHz Test procedure: ANSI C63.4, Sections 8.3.2, 13.2, 13.4 Test mode: Compliance
Test specification: Section 15.253(e)(1), Radiated emissions below 40 GHz Test procedure: ANSI C63.4, Sections 8.3.2, 13.2, 13.4 Plot 7.2.7 Radiated emission measurements at frequency 7280 MHz Low channel
More informationARE STAR CONTRIBUTION NETWORKS MORE BANDWIDTH EFFICIENT THAN MESH NETWORKS?
ARE STAR CONTRIBUTION NETWORKS MORE BANDWIDTH EFFICIENT THAN MESH NETWORKS? Dirk Breynaert, Newtec 04 Augustus 2005 Abstract The article is mainly investigating the satellite bandwidth efficiency of MESH
More informationReport On. FCC and Industry Canada Testing of the Inmarsat Global Ltd IsatPhone Pro GMR2+ Satellite Phone COMMERCIAL-IN-CONFIDENCE
Report On FCC and Industry Canada Testing of the Inmarsat Global Ltd IsatPhone Pro GMR2+ Satellite Phone FCC ID: YCTISATPHONE IC ID: 8944A-ISATPHONE Document 75909459 Report 07 Issue 1 June 2010 TUV Product
More informationChapter 4 The RF Link
Chapter 4 The RF Link The fundamental elements of the communications satellite Radio Frequency (RF) or free space link are introduced. Basic transmission parameters, such as Antenna gain, Beamwidth, Free-space
More informationQDV120 Operation and Pointing manual
QDV120 Operation and Pointing manual MPAD1 Plus OP-080316-E1 page 1 Contents Item Description Page 1.0 Health and Safety for Operators and Installation Staff 3 2.0 Transit case Reflector/Mount/BUC/LNB
More informationLE/ESSE Payload Design
LE/ESSE4360 - Payload Design 4.3 Communications Satellite Payload - Hardware Elements Earth, Moon, Mars, and Beyond Dr. Jinjun Shan, Professor of Space Engineering Department of Earth and Space Science
More informationOfcom application form OfW453. Application for clearance of an earth station operating within a Satellite (Earth Station Network) Licence
Ofcom application form OfW453 Application for clearance of an earth station operating within a Satellite (Earth Station Network) Licence Please ensure this form is signed and dated at the bottom and use
More informationFIGURE 14-1 (a) Focal points F1 and F2, semimajor axis a, and semiminor b of an ellipse; (b) Kepler s second law
FIGURE 14-1 (a) Focal points F1 and F2, semimajor axis a, and semiminor b of an ellipse; (b) Kepler s second law FIGURE 14-2 Satellite orbits: (a) circular; (b) elliptical FIGURE 14-3 Satellite orbital
More informationTitle: Test on 5.8 GHz Band Outdoor WiFi (802.11b/g) Wireless Base Station
Page 20 of 51 Pages 7.5. Conducted spurious emission 7.5.1. Requirements: Clause 15.247(d). In any 100 khz bandwidth outside the frequency band in which the spread spectrum or digitally modulated intentional
More informationMELTEK INFOSYSTEMS PVT. LTD. VERTEX MAKE 9MTR ANTENNA I&C FOR DEAL DEHRADUN (BEL PROJECT)
MELTEK INFOSYSTEMS PVT. LTD. VERTEX MAKE 9MTR ANTENNA I&C FOR DEAL DEHRADUN (BEL PROJECT) Scope of Work 1. Vertex makes 9mtr Antenna Erection, Installation & commissioning and NOCC at DEAL Dehradun. 2.
More informationAve output power ANT 1(dBm) Ave output power ANT 2 (dbm)
Page 41 of 103 9.6. Test Result The test was performed with 802.11b Channel Frequency (MHz) power ANT 1(dBm) power ANT 2 (dbm) power ANT 1(mW) power ANT 2 (mw) Limits dbm / W Low 2412 7.20 7.37 5.248 5.458
More informationPoint-to-Multipoint Coexistence with C-band FSS. March 27th, 2018
Point-to-Multipoint Coexistence with C-band FSS March 27th, 2018 1 Conclusions 3700-4200 MHz point-to-multipoint (P2MP) systems could immediately provide gigabit-class broadband service to tens of millions
More informationFCC ID: A3LSLS-BD106Q. Report No.: HCT-RF-1801-FC003. Plot Data for Output Port 2_QPSK 9 khz ~ 150 khz Middle channel 150 khz ~ 30 MHz Low channel
Plot Data for Output Port 2_QPSK 9 khz ~ 150 khz Middle channel 150 khz ~ 30 MHz Low channel 30 MHz ~ 1 GHz Middle channel 1 GHz ~ 2.491 GHz Low channel 2.695 GHz ~ 12.75 GHz High channel 12.75 GHz ~ 26.5
More informationEMC Test Data. Radio Test Report R Summit Data Communications SDC-MCF10G. Test Report R76253 Rev 3.0. Revision History.
EMC Test Data Radio Test Report R76253 For The Summit Data Communications Model SDC-MCF10G Revision History Rev # Made By Date Comments 1.0 Mark Hill 31-Jul-09 Initial Release 2.0 Mark Briggs 11-Aug-09
More informationKa by C-COM Satellite Systems Inc.
Ka-66 The inetvu Ka-66 Drive-Away Antenna is a 66 cm auto-acquire satellite antenna system which can be mounted on the roof of a vehicle for direct broadband access over any configured satellite. The system
More informationETSI TS V1.1.1 ( )
TS 102 188-5 V1.1.1 (2004-03) Technical Specification Satellite Earth Stations and Systems (SES); Regenerative Satellite Mesh - A (RSM-A) air interface; Physical layer specification; Part 5: Radio transmission
More informationELECTRICAL TESTING
ELECTRICAL TESTING 0839.01 Hermon Laboratories Ltd. Harakevet Industrial Zone, Binyamina 30500, Israel Tel. +972-4-6288001 Fax. +972-4-6288277 E-mail: mail@hermonlabs.com TEST REPORT ACCORDING TO: FCC
More informationRF Emissions Test Report To Determine Compliance With: FCC, Part 15 Rules and Regulations
RF Emissions Test Report To Determine Compliance With: FCC, Part 15 Rules and Regulations Model numbers: HT130022 Rev. B. December 17, 2002 Manufacturer: HQ, Inc. 210 9th Steet Drive Palmetto, FL 34221
More informationCOORDINATION REQUEST. Capture Exercise
COORDINATION REQUEST Capture Exercise Coordination request for a new Chilean (CHL) GSO Satellite Network (1.12.2010) Identity of Satellite network: Nominal Orbital Longitude: ITUSAT 70 DEGREES WEST Longitudinal
More informationHigh Speed Data Downlink for NSF Space Weather CubeSats
High Speed Data Downlink for NSF Space Weather CubeSats National Science Foundation Meeting Monday August 31, 2009 Charles Swenson Satellite Data Flow Onboard Instruments R collected Spacecraft Memory
More informationRECOMMENDATION ITU-R S * Maximum permissible level of off-axis e.i.r.p. density from very small aperture terminals (VSATs)
Rec. ITU-R S.728-1 1 RECOMMENDATION ITU-R S.728-1 * Maximum permissible level of off-axis e. density from very small aperture terminals (VSATs) (1992-1995) The ITU Radiocommunication Assembly, considering
More informationPrecision Validation, Maintenance and Repair of Satellite Earth Stations
Precision Validation, Maintenance and Repair of Satellite Earth Stations September 18, 2014 Co-sponsored by Keysight Technologies 2014 Tom Hoppin Application Specialist Component Test Division Keysight
More informationDay 1 Session 2. Earth Station Technology
Day 1 Session 2 Earth Station Technology 1 1- Types of antennas Satellites being far from earth require directional antennas in order to communicate. A directional antenna normally uses a parabolic reflector
More informationFCC PART 95 MEASUREMENT AND TEST REPORT. Powerwerx, Inc.
FCC PART 95 MEASUREMENT AND TEST REPORT For Powerwerx, Inc. 23695 Via Del Rio Yorba Linda California 92887, United States FCC ID: 2ACK8TR505D Report Type: Original Report Product Type: Two-way radio Test
More informationFCC Part 22H & 24E Measurement and Test Report
FCC Part 22H & 24E Measurement and Test Report For Shenzhen Concox Information Technology Co., Ltd Floor 4th, Building B, Gaoxinqi Industrial Park, Liuxian 1st Road, District 67, Bao an, Shenzhen, China
More informationEutelsat S.A. Type Approval Certificate. Granted to. With Registration Number EA-V057. Eutelsat S.A. ROCKWELL COLLINS SWEDEN AB. F.
Eutelsat S.A. Type Approval Certificate Granted to ROCKWELL COLLINS SWEDEN AB With Registration Number F. Schurig Department for Satellite Missions and Programmes Eutelsat S.A. TYPE APPROVAL CERTIFICATE
More informationRECOMMENDATION ITU-R S.733-1* (Question ITU-R 42/4 (1990))**
Rec. ITU-R S.733-1 1 RECOMMENDATION ITU-R S.733-1* DETERMINATION OF THE G/T RATIO FOR EARTH STATIONS OPERATING IN THE FIXED-SATELLITE SERVICE (Question ITU-R 42/4 (1990))** Rec. ITU-R S.733-1 (1992-1993)
More informationHAM RADIO DELUXE SATELLITES A BRIEF INTRODUCTION. Simon Brown, HB9DRV. Programmer- in- C hief
HAM RADIO DELUXE SATELLITES A BRIEF INTRODUCTION Simon Brown, HB9DRV Programmer- in- C hief Last update: Sunday, September 26, 2004 User Guide The IC-703s and IC-7800s used in this project were supplied
More informationElectrical FOR:
839.01 Electrical Hermon Laboratories Ltd. Harakevet Industrial Zone, Binyamina 30500, Israel Tel. +972-4-6288001 Fax. +972-4-6288277 E-mail: mail@hermonlabs.com TEST REPORT ACCORDING TO: EN 300 113-2
More informationFCC 47 CFR PART 15 SUBPART C CERTIFICATION TEST REPORT FOR. Bluetooth Remote Control for Video Set Top Box MODEL NUMBER: IPRC1000 FCC ID: 2ABTE-L3YJC9
FCC 47 CFR PART 15 SUBPART C CERTIFICATION TEST REPORT FOR Bluetooth Remote Control for Video Set Top Box MODEL NUMBER: IPRC1000 REPORT NUMBER: 15U22448-E1V4 ISSUE DATE: 3/7/2016 Prepared for Verizon Online
More informationSatellite Communications
Satellite Communications Part IV-Lecture 3-Satellite Link Design Lecturer Madeeha Owais 1 Learning Objectives Solving calculations of Link Budget for various satellite systems 2 Design of Satellite Communication
More informationTable of Contents 1. GENERAL INFORMATION SYSTEM TEST CONFIGURATION CONDUCTED EMISSIONS TEST RADIATED EMISSION TEST...
Table of Contents 1. GENERAL INFORMATION... 4 1.1 PRODUCT DESCRIPTION FOR EQUIPMENT UNDER TEST... 4 1.2 RELATED SUBMITTAL(S) / GRANT (S)... 7 1.3 TEST METHODOLOGY... 7 1.4 EQUIPMENT MODIFICATIONS... 7
More informationSpace Frequency Coordination Group
Space Frequency Coordination Group Report SFCG 38-1 POTENTIAL RFI TO EESS (ACTIVE) CLOUD PROFILE RADARS IN 94.0-94.1 GHZ FREQUENCY BAND FROM OTHER SERVICES Abstract This new SFCG report analyzes potential
More informationRECOMMENDATION ITU-R SM * Measuring of low-level emissions from space stations at monitoring earth stations using noise reduction techniques
Rec. ITU-R SM.1681-0 1 RECOMMENDATION ITU-R SM.1681-0 * Measuring of low-level emissions from space stations at monitoring earth stations using noise reduction techniques (2004) Scope In view to protect
More informationDRC 3500 Versatile Ka-Band Transceiver
DRC 3500 Key Features: Flexible Polarisation: RHCP/ LHCP and cross/co-polar 2 GHz operation by switchable sub-bands Optimised, integrated Feed-chain for highest EIRP and G/T True 5 Watt P1dB at the Feed
More informationSTUDIO TO TRANSMITTER LINKING SYSTEM
RFS37 May 1995 (Issue 1) SPECIFICATION FOR RADIO LINKING SYSTEM: STUDIO TO TRANSMITTER LINKING SYSTEM USING ANGLE MODULATION WITH CARRIER FREQUENCY SEPARATION BETWEEN 75 AND 500 khz Communications Division
More informationHAM RADIO DELUXE SATELLITES A BRIEF INTRODUCTION. Simon Brown, HB9DRV. Programmer- in- C hief
HAM RADIO DELUXE SATELLITES A BRIEF INTRODUCTION Simon Brown, HB9DRV Programmer- in- C hief Last update: Sunday, November 30, 2003 User Guide The IC-703s used in this project were supplied by Martin Lynch
More informationGround System Training Department
Module 7: IPSTAR Uplink Access Test (IUAT) Ground System Training Department 2012-03-Standard (iuat1.14)-uti-101 THAICOM Public Company Limited Module Objectives At the end of the module the participant
More informationEUTELSATS.A. SYSTEMS OPERATIONS GUIDE. Volume II. ESOG Module 260 MANUAL AND AUTO-DEPLOY TERMINALS HANDBOOK. Issue
Volume II - ESOG Module 260 - Issue 2.1 MANUAL AND AUTO-DEPLOY TERMINALS HANDBOOK 10 October 2012 EUTELSATS.A. SYSTEMS OPERATIONS GUIDE ESOG Module 260 MANUAL AND AUTO-DEPLOY TERMINALS HANDBOOK Issue 2.1
More informationDouble-Ridged Waveguide Horn
Model 3106 200 MHz 2 GHz Uniform Gain Power Handling up to 1.6 kw Model 3115 1 GHz 18 GHz Low VSWR Model 3116 18 GHz 40 GHz Quality Construction M O D E L 3 1 0 6 Double-Ridged Waveguide Horn PROVIDING
More informationRadiated Spurious Emission Testing. Jari Vikstedt
Radiated Spurious Emission Testing Jari Vikstedt jari.vikstedt@ets-lindgren.com What is RSE? RSE = radiated spurious emission Radiated chamber Emission EMI Spurious intentional radiator 2 Spurious Spurious,
More informationFCC 47 CFR PART 15 SUBPART C CERTIFICATION TEST REPORT FOR. RF ID Reader MODEL NUMBER: A-405 FCC ID: WFQITCS-A-405 IC: 10717A-ITCSA405
FCC 47 CFR PART 15 SUBPART C CERTIFICATION TEST REPORT FOR RF ID Reader MODEL NUMBER: A-405 REPORT NUMBER: 10906664A ISSUE DATE: December 12, 2015 Prepared for RF Controls LLC 1400 S 3 RD Street Suite
More information4GHz / 6GHz Radiation Measurement System
4GHz / 6GHz Radiation Measurement System The MegiQ Radiation Measurement System (RMS) is a compact test system that performs 3-axis radiation pattern measurement in non-anechoic spaces. With a frequency
More informationGlossary of Satellite Terms
Glossary of Satellite Terms Satellite Terms A-D The following terms and definitions will help familiarize you with your Satellite solution. Adaptive Coding and Modulation (ACM) Technology which automatically
More informationScalable Ionospheric Analyser SIA 24/6
Scalable Ionospheric Analyser SIA 24/6 Technical Overview Functional description The ATRAD Scalable Ionospheric Analyser SIA24/6 is designed to observe ionospheric irregularities and their drift in the
More information9. MAXIMUM CONDUCTED OUTPUT POWER SPECTRAL DENSITY
9. MAXIMUM CONDUCTED OUTPUT POWER SPECTRAL DENSITY 9.1. MEASUREMENT PROCEDURE (1). Connect EUT RF output port to the Spectrum Analyzer through an RF attenuator (2). Set the EUT Work on the top, the middle
More information1.8M Transportable SNG Antenna
1.8M Transportable SNG Antenna Model CZ-180 C band SNG antenna have been developed and manufactured by SUNCOM for emergency mobile satellite communication. The systems feature in highly intelligentized,
More information2310 to 2390 MHz, 3m distance MCS8 (MIMO) to 2500 MHz Restricted band MCS8 (MIMO)
2310 to 2390 MHz, 3m distance MCS8 (MIMO) Lower band edge, Average (Low Channel) Lower band edge, Peak (Low Channel) 2483.5 to 2500 MHz Restricted band MCS8 (MIMO) Upper band edge, Peak (High Channel)
More informationSatellite TVRO G/T calculations
Satellite TVRO G/T calculations From: http://aa.1asphost.com/tonyart/tonyt/applets/tvro/tvro.html Introduction In order to understand the G/T calculations, we must start with some basics. A good starting
More informationSATELLITE SUBSYSTEMS. Networks and Communication Department. Dr. Marwah Ahmed
1 SATELLITE SUBSYSTEMS Networks and Communication Department Dr. Marwah Ahmed Outlines Attitude and Orbit Control System (AOCS) Telemetry, Tracking, Command and Monitoring (TTC & M) Power System Communication
More informationSPACEX NON-GEOSTATIONARY SATELLITE SYSTEM
SPACEX NON-GEOSTATIONARY SATELLITE SYSTEM ATTACHMENT A TECHNICAL INFORMATION TO SUPPLEMENT SCHEDULE S A.1 SCOPE AND PURPOSE This attachment contains the information required under Part 25 of the Commission
More informationTRANSMITTER MODEL: KAS-2030M
Page 1 of 16 FCC PART 15, SUBPART B and C TEST REPORT for TRANSMITTER MODEL: KAS-2030M Prepared for WILDLIFE TECHNOLOGIES 115 WOLCOTT STREET MANCHESTER, NEW HAMPSHIRE 03103 Prepared by: KYLE FUJIMOTO Approved
More informationCoordination and Analysis of GSO Satellite Networks
Coordination and Analysis of GSO Satellite Networks BR-SSD e-learning Center BR / SSD / SNP 1 Summary: 1) How to Identify Satellite Networks and other Systems for which Coordination is Required? 2) Several
More informationUNIVERSITY OF NAIROBI Radio Frequency Interference in Satellite Communications Systems
UNIVERSITY OF NAIROBI Radio Frequency Interference in Satellite Communications Systems Project No. 090 Mitei Ronald Kipkoech F17/2128/04 Supervisor: Dr.V.K Oduol Examiner: Dr. Gakuru OBJECTIVES To study
More informationAnnex B: HEO Satellite Mission
Annex B: HEO Satellite Mission Table of Content TABLE OF CONTENT...I 1. INTRODUCTION...1 1.1. General... 1 1.2. Response Guidelines... 1 2. BRAODBAND CAPACITY...2 2.1. Mission Overview... 2 2.1.1. HEO
More information7. FREQUENCY SEPARATION
7. FREQUENCY SEPARATION 7.1. Limits According to FCC Section 15.247(a)(1), Frequency hopping systems shall have hopping channel carrier frequencies separated by a minimum of 25 khz or two-thirds of the
More informationTest Report. Prepared for: Wilson Electronics, Inc. Model: Description: Dual Band In-Building Signal Booster FCC ID: PWO
Test Report Prepared for: Wilson Electronics, Inc. Model: 460005 Description: Dual Band In-Building Signal Booster FCC ID: PWO460005 To FCC Part 20 Date of Issue: January 27, 2014 On the behalf of the
More informationTEST REPORT FROM RADIO FREQUENCY INVESTIGATION LTD.
TEST REPORT FROM RADIO FREQUENCY INVESTIGATION LTD. Test Of: Wood & Douglas Ltd ST500 Transmitter Test Report Serial No: RFI/EMCB2/RP39403B This Test Report supersedes RFI Test Report No.: RFI/EMCB1/RP39403B
More informationRECOMMENDATION ITU-R S.1340 *,**
Rec. ITU-R S.1340 1 RECOMMENDATION ITU-R S.1340 *,** Sharing between feeder links the mobile-satellite service and the aeronautical radionavigation service in the Earth-to-space direction in the band 15.4-15.7
More informationSpectrian Dual Mode Cellular Power Amplifier Model No.: SCLPA 800 CR FCC ID: I2ONTHX51AA
A Class II Permissive Change - FCC Part 22 Type Acceptance Test Report for Spectrian Dual Mode Cellular Power Amplifier Model No.: SCLPA 800 CR FCC ID: I2ONTHX51AA Date of Report: May 26, 1999 Total No.
More informationM2 Antenna Systems, Inc. Model No:
M2 Antenna Systems, Inc. Model No: 400-600-10 SPECIFICATIONS: Model... 400-600-10 Frequency Range... 390 To 650 MHz *Gain... 12 To 13 dbic Front to back... 20 db Nominal Beamwidth... 46 Nominal Feed Impedance....
More informationFor Sky. Phone LLC. FCC Part 22H. FCC Rules: 3G Smart Phone. Report No.: By: Tested By: Manager. Prepared. Shenzhen SEM.
FCC Part 22H & 24E Measurement and Test Report For Sky Phone LLC 1348 Washington Av. Suite 350, Miamii Beach, Florida, F United States FCCC ID: 2ABOSSKYPLATA55 FCC Rules: Product Description: Tested Model:
More informationAPPENDIX A TEST PLOTS. (Model: 15Z970)
APPENDIX A APPENDIX A TEST PLOTS (Model: 15Z970) APPENDIX A-Page 1 of 36 TABLE OF CONTENTS A.1 6dB BANDWIDTH MEASUREMENT... 2 A.1.1 6dB Bandwidth Result... 2 A.1.2 Measurement Plots... 3 A.2 MAXIMUM PEAK
More informationFCC Test Report. Report No.: AGC FE02 CLIENT : INNOVATIVE CONCEPTS AND DESIGN LLC. Attestation of Global Compliance (Shenzhen) Co., Ltd.
Page 1 of 43 FCC Test Report Report No.: AGC03588150607FE02 FCC ID : 2AE6GUHF 6000HHM APPLICATION PURPOSE : ORIGINAL EQUIPMENT PRODUCT DESIGNATION : Wireless Microphone BRAND NAME : Gemini MODEL NAME :
More informationEarth Station Coordination
1 Overview Radio spectrum is a scarce resource that should be used as efficiently as possible. This can be achieved by re-using the spectrum many times - having many systems operate simultaneously on the
More informationRadio compliance test
Training Course on radio measurement June 2016 Radio compliance test Presented by: Karim Loukil & Afef Bohli Page 1 Radio equipement An electrical or electronic product or an interface that intentionally
More information1.0 Job Description 1.1 Client Information This EUT has been tested at the request of: Company: Spectronic Denmark A/S Contact: John Herlev Telephone: 011 45 863-87-222 Fax: 011 45 863-87-704 Email: jhe@spectronic-denmark.com
More informationACCORDING TO: FCC part 15 subpart C, and subpart B FOR:
Electrical Hermon Laboratories Ltd. P.O.Box 23, Binyamina 30500, Israel Tel. +972 4628 8001 Fax. +972 4628 8277 E-mail: mail@hermonlabs.com TEST REPORT ACCORDING TO: FCC part 15 subpart C, 15.247 and subpart
More informationMEASUREMENT PROCEDURE AND TEST EQUIPMENT USED
MEASUREMENT PROCEDURE AND TEST EQUIPMENT USED Except where otherwise stated, all measurements are made following the Electronic Industries Association (EIA) Minimum Standard for Portable/Personal Land
More informationRECOMMENDATION ITU-R S.524-6
Rec. ITU-R S.524-6 1 RECOMMENDATION ITU-R S.524-6 MAXIMUM PERMISSIBLE LEVELS OF OFF-AXIS e.i.r.p. DENSITY FROM EARTH STATIONS IN GSO NETWORKS OPERATING IN THE FIXED-SATELLITE SERVICE TRANSMITTING IN THE
More informationME7220A. Radar Test System (RTS) Target Simulation & Signal Analysis for Automotive Radar Exceptional Performance at an Affordable Price.
ME7220A Test System (RTS) 76 to 77 GHz Target Simulation & Signal Analysis for Automotive Exceptional Performance at an Affordable Price The Challenge The installation of collision warning and Adaptive
More informationELECTRONIC FILING for EARTH STATION (Art 9 & 11)
ELECTRONIC FILING for EARTH STATION (Art 9 & 11) Info Two steps to be followed Coordination Submission of Appendix 4 data to affected ADM s Notification Submission of Appendix 4 data to BR 3 Why you need
More informationUsing Frequency Diversity to Improve Measurement Speed Roger Dygert MI Technologies, 1125 Satellite Blvd., Suite 100 Suwanee, GA 30024
Using Frequency Diversity to Improve Measurement Speed Roger Dygert MI Technologies, 1125 Satellite Blvd., Suite 1 Suwanee, GA 324 ABSTRACT Conventional antenna measurement systems use a multiplexer or
More informationThe Discussion of this exercise covers the following points:
Exercise 3-2 Frequency-Modulated CW Radar EXERCISE OBJECTIVE When you have completed this exercise, you will be familiar with FM ranging using frequency-modulated continuous-wave (FM-CW) radar. DISCUSSION
More informationANTENNA SYSTEMS. 1.8m Offset Rx & TxRx Antenna INSTALLATION & ASSEMBLY INSTRUCTIONS
ANTENNA SYSTEMS.m Offset Rx & TxRx Antenna INSTALLATION & ASSEMBLY INSTRUCTIONS LIMITED TWELVE () MONTH WARRANTY This PATRIOT ANTENNA equipment is warranted to be free from defects in material and workmanship
More informationBROADBAND AND HIGH GAIN OMNIS
C WDA series antennas are optimized for both broadband and high gain performance. These antennas are ideally suited for use with frequency hopping radios and wideband jammers where tuning or band switching
More informationB ==================================== C
Satellite Space Segment Communication Frequencies Frequency Band (GHz) Band Uplink Crosslink Downlink Bandwidth ==================================== C 5.9-6.4 3.7 4.2 0.5 X 7.9-8.4 7.25-7.7575 0.5 Ku 14-14.5
More informationEs'hail-2 (P4-A) the first geostationary OSCAR from Qatar. Peter Gülzow, DB2OS AMSAT-DL President
Es'hail-2 (P4-A) the first geostationary OSCAR from Qatar Peter Gülzow, DB2OS AMSAT-DL President AMSAT Symposium Reno 2017 AMSAT Phase 4 Hosted Amateur Radio Payload (AMSAT P4-A): S-Band uplink / X-Band
More informationECC Recommendation (16)04
ECC Recommendation (16)04 Determination of the radiated power from FM sound broadcasting stations through field strength measurements in the frequency band 87.5 to 108 MHz Approved 17 October 2016 Edition
More informationMeasurement Procedure & Test Equipment Used
Measurement Procedure & Test Equipment Used Except where otherwise stated, all measurements are made following the Electronic Industries Association (EIA) Minimum Standard for Portable/Personal Land Mobile
More informationDescription of Test Facility
Description of Test Facility Name: Address: Intertek Testing Services Limited Shanghai Building No.86, 1198 Qinzhou Road(North), Shanghai 200233, P.R. China FCC Registration Number: 236597 IC Assigned
More informationRECOMMENDATION ITU-R S.1063 * Criteria for sharing between BSS feeder links and other Earth-to-space or space-to-earth links of the FSS
Rec. ITU-R S.1063 1 RECOMMENDATION ITU-R S.1063 * Criteria for sharing between BSS feeder links and other Earth-to-space or space-to-earth links of the FSS (Question ITU-R 10/) (199) The ITU Radiocommunication
More informationFCC CFR47 PART 15 SUBPART C INDUSTRY CANADA RSS-247 ISSUE 1 BLUETOOTH LOW ENERGY CERTIFICATION TEST REPORT FOR
FCC CFR47 PART 15 SUBPART C INDUSTRY CANADA RSS-247 ISSUE 1 BLUETOOTH LOW ENERGY CERTIFICATION TEST REPORT FOR WLAN 2X2 MIMO 802.11a/b/g/n/ac with BLUETOOTH MODEL NUMBER: P2180 REPORT NUMBER: 15U21878-E2V1
More informationARTICLE 22. Space services 1
CHAPTER VI Provisions for services and stations RR22-1 ARTICLE 22 Space services 1 Section I Cessation of emissions 22.1 1 Space stations shall be fitted with devices to ensure immediate cessation of their
More informationEEG 816: Radiowave Propagation 2009
Student Matriculation No: Name: EEG 816: Radiowave Propagation 2009 Dr A Ogunsola This exam consists of 5 problems. The total number of pages is 5, including the cover page. You have 2.5 hours to solve
More informationGUIDELINES FOR THE APPLICATION FOR A SPACE STATION CARRIER LICENCE. Section 1 - Introduction
GUIDELINES FOR THE APPLICATION FOR A SPACE STATION CARRIER LICENCE Section 1 - Introduction 1.1 Pursuant to section 7(5) of the Telecommunications Ordinance (hereinafter the Ordinance ), the Communications
More informationRADIO: FORM TC004 APPLICATION FOR SPECTRUM LICENCE IN AMATEUR, RADIODETERMINATION AND SATELLITE SERVICES. Provisions of the Telecommunication Act 2009
Explanatory Notes: Please read this information and the notes at the back of this form before completing the application You may use this form only for the type of licences shown in Section D. If space
More information