What would you like to do ? -------------------------- Help us find the most requested user's guides Upload your
user manual Search for a user manual Register Login and access your manuals Reset your password

	Browse all user guides
	The RAYSTAR 112 GPS product forum
	Upload your user manual
	Sign-up Log in
	Help us find the most requested user's guides
	Include the add-on to download manuals from your site, forum or blog
	Frequently Asked Questions
	Contact Diplodocs team
ALL GUIDES BY CATEGORY Domestic Appliance TV & Audio Car & Motorcycle Phone Computer Camera & Video Music Sport Gardening & Housekeeping Video Game & Software Jewelry & Watch Baby & Toys Hygiene & Health Other

Distributed by Any reference to Raytheon or RTN in this manual should be interpreted as Raymarine. The names Raytheon and RTN are owned by the Raytheon Company. GPS SENSOR OPERATION MANUAL RAYSTAR 112 Installation and Operation Handbook RAYSTAR 112 GPS SENSOR Owner/Installation Manual PURPOSE This manual contains very important information on the installation, operation, and maintenance of your new equipment. In order to get the best results in operation and performance, please take the time to read this manual thoroughly. IMPORTANT NOTICE This device is only an aid to navigation. Its accuracy can be affected by many factors, including equipment failure or defects, environmental conditions and improper handling or use. It is the user's responsibility to exercise common prudence and navigational judgement, and this device should not be relied upon as a substitute for such prudence and judgement. RAYTHEON ELECTRONICS products are supported by a network of Authorized Service Representatives. For information on Raytheon products and services, contact any of the following: UNITED STATES Raytheon Marine Company 676 Island Pond Road Manchester, N.H. 03109 ­ 5420 Telephone: (603) 647 ­ 7530 Facsimillie: (603) 634 ­ 4756 Raytheon Marine Europe Limited Anchorage Park Portsmouth Hampshire PO3 5TD United Kingdom. Telephone: 44 ­ 1705 693611 Facsimillie: 44 ­ 1705 694642 EUROPE ã Copyright Raytheon Electronics 1997 The technical and graphical information contained in this handbook, to the best of our knowledge, was correct as it went to press. However, the Raytheon policy of continuous improvement and updating may change product specifications without prior notice. Therefore, unavoidable differences between the product and handbook may occur from time to time, for which liability cannot be accepted by Raytheon. RAYSTAR 112 Installation and Operation Handbook RAYSTAR 112 Installation and Operation Handbook EMC Installation & Service Guidelines IMPORTANT NOTE All Raytheon equipment and accessories are designed to the best industry standards for use in the leisure marine environment. Their design and manufacture conforms to the Electromagnetic Compatibility (EMC) Regulations, but good installation is required to ensure that performance is not compromised. Although every effort has been taken to ensure that they will perform under all conditions, it is important to understand what factors could affect the operation of the product. Installation To avoid the risk of operating problems, all Raytheon equipment and cables connected to it should be; · At least 1m (3 ft) from any equipment transmitting or cables carrying radio signals e.g. VHF radios, cables and antennas. In the case of SSB radios, the distance should be increased to 2m (7ft). · More than 2m (7ft) from the path of a radar beam. A radar beam can normally be assumed to spread 20 degrees above and below the radiating element. · The equipment should be supplied from a different battery than the one used for engine start. Voltage drops below 10v in the power supply to our products can cause the equipment to reset. This will not damage the equipment, but will cause the loss of some information and can change the operating mode. · Genuine Raytheon cables should be used at all times. Cutting and rejoining these cables can compromise EMC performance and so should be avoided unless doing so is detailed in the installation manual. RAYSTAR 112 Installation and Operation Handbook Check Before Going to Sea · Always check the installation before going to sea to make sure that it is not affected by radio transmissions, engine starting etc.. · In some installations, it may not be possible to prevent the equipment from being affected by external influences. In general this will not damage the equipment but can lead to it resetting, or momentarily may result in faulty operation. Servicing and Safety · Raytheon equipment should be serviced only by authorised Raytheon service engineers. They will ensure that service procedures and replacement parts used will not affect performance. There are no user serviceable parts in any Raytheon product. · Some products generate high voltages, and so never handle the cables/connectors when power is being supplied to the equipment. · Always report any EMC related problem to your nearest Raytheon dealer. We will use any such information to improve our quality standards. Please keep these notes for future reference. Contents Contents Chapter1: Introduction ......................................................... 1 1.1 General Information .......................................................... 1 1.2 Basic GPS Information ...................................................... 1 Chapter 2: Installation ........................................................... 5 2.1 Installing the Sensor Unit ................................................... 5 2.1.1 Tips on Locating the Sensor ...................................... 5 2.1.2 Items Supplied .......................................................... 6 2.1.3 Mounting the Sensor ................................................. 6 2.2 Sensor Connections ......................................................... 7 DC Power ..................................................................... 7 NMEA 0183 Data Output ............................................... 7 Data Input to Sensor ..................................................... 8 2.2.1 Connection to Raytheon Units ................................... 8 2.2.2 Connections to DGPS Receiver ................................ 8 2.2.3 Connection to External Navigation Equipments .......... 9 2.2.4 Connection Diagram ............................................... 10 Chapter 3: Operation .......................................................... 11 3.1 COLD Start (Initial Start-up) ............................................. 11 3.2 Geodetic Datum ............................................................. 11 Chapter 4: Maintenance ...................................................... 13 4.1 General .......................................................................... 13 4.2 Replacing the Battery ...................................................... 13 4.3 Trouble Shooting ............................................................ 14 4.4 Electrical Specifications: .................................................. 15 General: .......................................................................... 15 Mechanical Specifications: ............................................... 15 RAYSTAR 112 Installation and Operation Handbook Appendix A ......................................................................... 17 Additional Local Geodetic Systems .................................. 17 Chapter 1: Introduction 1 Chapter1: Introduction 1.1 General Information Congratulations on your purchase of Raytheon's Raystar 112 GPS sensor unit. We think you will appreciate the accuracy of GPS, the quality, long-term reliability, and additional space saving convenience of having GPS navigation data available at your navigation console from your new Raystar 112. Built into the environmentally rugged, compact housing is our newest 12 channel GPS receiver/processor combined with the ADP antenna. The position output data from the Raystar 112 can be displayed on radars, plotters, fishfinders, lorans, and other navigation equipment capable of accepting NMEA 0183 formatted data. 1.2 Basic GPS Information GPS is a satellite-based radionavigation system developed and operated by the U.S. Department of Defense (DOD). GPS permits land, sea and airborne users to determine their three-dimensional position, velocity, and time 24 hours a day, in all weather, anywhere in the world with a precision and accuracy far better than other radionavigation systems available today or in the forseeable future. GPS consists of three segments: space, control and user. The Space Segment, consists of 24 operational satellites in six circular orbits 20,200 km (10,900 nm) above the earth at an inclination angle of 55 degrees with a 12 hour period. The satellites are spaced in orbit so 2 RAYSTAR 112 Installation and Operation Handbook that at any time a minimum of 6 satellites will be in view to users anywhere in the world. The satellites continuously broadcast position and time data to users throughout the world. The Control Segment, consists of a master control station in Colorado Springs, with five monitor stations and three ground antennas located throughout the world. The monitor stations track all GPS satellites in view and collect ranging information from the satellite broadcasts. The monitor stations send the information they collect from each of the satellites back to the master control station, which computes extremely precise satellite orbits. The information is then formatted into updated navigation messages for each satellite. The updated information is transmitted to each satellite via the ground antennas, which also transmit and receive satellite control and monitoring signals. The User Segment consists of the receivers, processors, and antennas that allow land, sea, or airborne operators to receive the GPS satellite broadcasts and compute their precise position, velocity and time. The satellites continuously broadcast their navigation messages at a frequency of 1575.42 Mhz (for civilian use). Superimposed on the navigation message is a high rate coarse acquisition (C/A) code used for precise positioning measurements and positive satellite identification. The C/A ID code permits the user to identify particular satellites and, in some cases, to determine and select the "best satellites" to use in position calculations. If it were possible to measure true satellite ranges directly, it would only be necessary to track data from any two satellites to obtain a vessel's latitude/longitude. In actual practice, for marine navigation, the receiver must lock onto and track a minimum of three satellites in order to resolve timing errors, including the receiver's own internal clock timing bias error which must be factored into the various range calculations. Chapter 1: Introduction 3 Normally the Raystar 112 tracks up to 12 satellites (if visible) and uses all tracked satellites for calculating position fixes. By using these satellites, the processor can determine the amount of clock errors in each range calculation. The receiver subtracts the error bias equally from each range solution until the lines of position (LOP's) intersect. Theoretically, this process can produce highly accurate latitutde/ longitude (L/L) position fixes for navigation within +/- 15m (rms). Continuous tracking of each satellite allows the receiver to perform this timing adjustment process and to calculate accurate measurements to the satellites. The Raystar 112 uses a 12 channel receiver. This sensor design method provides fast efficient acquisition and accurate position updating, even when satellites are obstructed from view. The US Department of Defense, for security reasons, has included a special mode in the GPS satellite system design which introduces variable timing errors into the satellite signals. This mode is known as "Selective Availability" (SA), and when it is enabled, is designed to provide less accurate fixes for all users (except military users). Accuracy in the order of +/- 100 Meters (rms) 95% of the time is obtained when SA is ON. This means that 95% of the time the actual ship's GPS Lat/ Long position will be within a radius of 100 meters (+/- one football field) and 5% of the time the actual position will be out of this 100 meter circle. Selective Availability has been enabled almost continuously since early 1991. The use of Differential GPS technology can remove most of these intentionally induced errors in the GPS satellite signals due to the "Selective Availiblity" mode including errors that can result due to environmental conditions as the satellite signals travel to earth.When you attach Raytheon's Differential Beacon Receiver to the Raystar 112 GPS sensor, the GPS differential corrections can improve the L/L 4 RAYSTAR 112 Installation and Operation Handbook position output accuracy of the Raystar 112 from +/- 100 meters down to 5 to 8 meters in most cases. The Raystar 112 provides NMEA 0183 formatted data at its output as follows: RMC GLL VTG GGA GSA GSV Combines position, course, and speed Vessel's Latitude/Longitude position Course over the ground, Speed over ground Ships L/L position & satellite status information Active satellites and DOP Satellites in view This data can be supplied to plotters, fishfinders, radars, integrated systems, etc., which are set up to use these sentences from the NMEA 0183 format. Please read through this manual thoroughly before proceeding with the installation and operation of the sensor. There are some important recommendations regarding successful installation practices to follow for getting the best GPS sensor performance. In the back of this manual you will also find a warranty registration card for your Raystar 112. To ensure that your unit is registered for full warranty coverage, please take a few moments to fill in the necessary information, and return the card to Raytheon. No postage is required if the card is mailed in the USA. Chapter 2: Installation 5 Chapter 2: Installation 2.1 Installing the Sensor Unit 2.1.1 Tips on Locating the Sensor The sensor is designed to receive the signals emitted from the satellites in a direct path. Ideally, the antenna unit should be mounted vertically in a location that is open and clear of any masts, search lights, or other structures that could block the line-of-sight reception of the antenna unit. The height of the GPS sensor is not as important as the sensor having a clear view horizon to horizon for ideal signal reception. In fact, the lower the antenna can be mounted and have a clear view to satellites, the better. The more stable the antenna, the easier it is to track satellites lower to the horizon. On sailboats, mounting the GPS to mast tops should generally be avoided. The GPS sensor should be separated by at least 3 ft (1m) from other communication antennas and should not be mounted in the direct path of the radar's antenna beam. While planning the location for the sensor, consider finding a convenient pathway for running the interconnecting cable which will connect the GPS sensor to the GPS display unit. Ideally the cable should be run in a manner so it can be hidden from view and, if possible, be in a direct path 6 RAYSTAR 112 Installation and Operation Handbook to the point of connection. It is important to keep the cable separated from other shipboard cables as much as possible to prevent interference pickup. 2.1.2 Items Supplied 1 each Raystar 112 GPS Sensor Unit, with 33ft (10 m) cable 1 each Instruction Manual 2.1.3 Mounting the Sensor The aluminum base of the sensor is threaded for use with a standard 1inch x 14 NPT marine antenna mount or extension mast. The base of the sensor has a slot cut into it so that the prewired cable can be fed externally of the mount or extension mast if so desired. If the connector is removed, the cable can be fed down through the extension mast or mount, exiting through the mount assembly. The aluminium base of your Raystar 112 Sensor has received a chromation treatment which adds toughness, resistance to wear and tear, and resistance to corrosion of the assembly. Prior to attaching the GPS sensor to the mount, we do recommend that a light coating of the silicon grease be applied th the surface of the threads of the sensor and mount. Screw the antenna onto the mount fully by hand while paying attention to avoid curling, tight loops, and kinking of the cable. When the unit is fully threaded on the mount use a proper sized spanner wrench and protective cloth to grip the base and snug the sensor to the mount. If the cable is fed internally through an extension mast, it is recommended that the cable slot in the sensor base assembly be sealed with RTV silicon sealant as protection from the environment. If Chapter 2: Installation 7 the cable is fed externally through the slot, the cable should be tyrapped or clamped at the base. Then the slot in the base should be sealed with RTV silicon sealant. The cable assembly supplied is 33 ft (10 m) in length with a 6 pin connector installed at the receiver end. The cable should be run as directly as possible to the navigation console or to the external navigation device. The cable may either be cut as necessary to the desired length or coiled and stored out of the way. If the cable is cut to length, the cable may be rejoined by following the connection diagram in section 2.2.4. 2.2 Sensor Connections The Raystar 112 sensor has the following input/output requirements: DC Power The 12 VDC power input to the sensor should be in the range of 11 to 16 VDC. It is important to verify that these voltage limits will not be exceeded to protect the GPS sensor unit. The negative leg of the 12V is grounded at the sensor base. If the vessel has a floating 12VDC system, an insulator must be used between the sensor base and mount to isolate the sensor from the ships ground. NMEA 0183 Data Output The NMEA 0183 Data contains RMC, GLL, VTG, GGA, GSA and GSV sentences. Please note that the sensor output is guaranteed to drive only 2 (two) devices directly. When using modern low current NMEA 0183 listener devices, up to 5 units can be driven in parallel. Contact your dealer if there are any questions regarding interfacing capabilities. 8 RAYSTAR 112 Installation and Operation Handbook Data Input to Sensor The sensor data input line is used to provide initialization data to the sensor unit as well as other set-up information, such as geodetic datum selection. This data is ordinarily provided via Raytheon's GPS display units (RayNav 298, RayNav 398, etc.). 2.2.1 Connection to Raytheon Units When the Raystar 112 sensor is connected directly to one of Raytheon's GPS display units, it normally obtains its 12VDC operating power input from the unit. In this typical installation, the 6 pin sensor connector is plugged directly into the connector labeled "GPS" on the rear of the display unit cabinet. The DC power is then supplied via pins 1 and 2 of the GPS connector to the sensor. Other external equipment requiring GPS data input should obtain their required NMEA 0183 data via connection to the data output wires located in the NAV display unit power cable assembly. 2.2.2 Connections to DGPS Receiver The Raystar 112 is designed to accept differential corrections in the RTCM Version 2.1 format from the Raytheon DGPS Beacon Receiver. The corrections from the Beacon receiver pass directly to the GPS sensor. A convenient "Y" cable assembly is packaged with the Beacon receiver to permit this interconnection. The diagram below shows the configuration. Chapter 2: Installation 9 2.2.3 Connection to External Navigation Equipments The diagram shown below should be followed to make connections of the NMEA 0183 data to external units. A terminal strip would provide a convenient means for attaching the necessary inputs and outputs. WARNING: OBSERVE PROPER POLARITY! The 12VDC power leads should normally be routed to the ship's DC power distribution panel on larger boats. The unit draws approximately 0.25 amps, so connection to a circuit breaker rated at 5 amps or less is recommended. On smaller vessels the power leads should be connected to a panel switch or to the main battery isolation switch or breaker. For best noise immunity from other shipboard electronics, avoid grouping the GPS sensor power connections together with the radar, radio, or echo sounder power leads on the same circuit breaker, if possible. The GPS's wiring should be separated as much as possible from these other devices. When using the NMEA 0183 format, the Raystar 112 can provide data for at 2 or more navigation equipments when connected in parallel. Be sure that all devices connected to the data output ( plotters, video sounders, radars) are programmed to use the NMEA 0183 data format. WARNING: Do NOT GROUND the Data, Data return lines, or the Shield of the interface cable at any of the external navigation equipments. Interface between equipments is normally completed by using a two wire, twisted pair, shielded, cable. If you are using a terminal strip as 10 RAYSTAR 112 Installation and Operation Handbook shown in the previous drawing, connect the Data ( + ) wire to terminal 4 of the terminal strip. Connect the Data return ( - ) wire to terminal 3. The shield of the interface cable is also connected to terminal 3 of the strip. 2.2.4 Connection Diagram Chapter3:Operation 11 Chapter 3: Operation 3.1 COLD Start (Initial Start-up) Your GPS is set up for fully Automatic operation when it leaves the factory. All you need to do is turn the unit ON. When power is applied to the Raystar 112 for the very first time, the GPS sensor has to locate and identify three or more satellites before determining the vessel's actual L/L position. The sensor's memories contain pre-programmed profiles of each satellite's signal coding. So it becomes a matter of sampling the incoming GPS signals and comparing the profiles until the signal coding matches. Unfortunately, this process (similiar to matching fingerprints) is both time consuming and complex. It can take up to 10 minutes before the unit completes satellite identification and calculates the first position. If you are using one of Raytheon's GPS display units, the operator can aid the GPS sensor in its satellite search by entering specific initialization information concerning ship's position, date, and time. The time required for obtaining the initial position fix can be reduced to approximately 1 to 3 minutes once the sensor has received this initialization data. After the sensor has completed this initial search and determined its location, the sensor will remember the L/L position in memory. The next time you use the unit, the only thing you'll have to do is turn the unit ON. In a few minutes your position will be displayed. This will occur as long as the ship remains within approximately 100 NMof the L/L position where the unit was turned OFF. If the vessel has been moved a substantial distance from the last saved position and the GPS sensor is then powered up, the unit may again go through the Cold Start routine. The time to acquire the satellites and get your position can be reduced by re-entering your new L/L position, date, and time information. 3.2 Geodetic Datum The normal Geodetic datum used by the Raystar 112 sensor is WGS-84. Mariners can/may find considerable errors (up to 200 m) in plotting own ship's position if their charts were created using one type of geodetic 12 RAYSTAR 112 Installation and Operation Handbook data system while the GPS sensor is busy calculating positions using another data system. When using the Raytheon's GPS display unit, the sensor can be programmed to use different geodetic datums for making position calculations. The datums that may be selected via the display unit are as follows: No. 0 1 2 3 4 5 6 7 8 9 Datum Area WGS-84 WGS-72 BESSEL NAD-27 NAD-27 CAN EUROPEAN 50 AUSTRAL 66 OSGB 36 NAD 83 Other Datums Service Area Default GPS datum Loran C Japan USA (older NOAA charts) Canada/Alaska Europe Australia UK (British Admiralty) USA see Appendix A When a sensor is programmed for a different datum, the datum will be saved in the sensors internal memory, which is backed-up by internal battery. If operating this unit with other navigation equipment, refer to the equipment users manual for instructions on set-ups or programming to select and receive external data inputs into those equipments. Chapter 4: Maintenance 13 Chapter 4: Maintenance 4.1 General Maintaining satisfactory operation of your Raystar 112 can depend on how well you care for the equipment. The simple maintenance tips that follow can save you time and money, as well as prevent unnecessary premature failures when the unit is most needed. Note: Periodically check system hardware. Inspect the sensor, mount, and cables, making sure all components are free of corrosion and are securely mounted. Examine the cable for evidence of chafing or abrasions. Clean and/or repair as necessary. Make sure connections to the ship's DC power are clean and tight. A light coating of a high insulation silicon grease (such as Dow Corning DC-4) can be used on connector pins to protect the plug contacts from corrosion when used. 4.2 Replacing the Battery The Raystar 112 contains internal memories to store your position, and other set-up information. A Lithium battery back-up keeps this memory information intact even when the unit is disconnected from the ship's battery. The estimated life span of the battery is five years. If the battery should fail, the memory contents will be lost. While the Raystar 112 will still operate without the battery, the unit will take longer to acquire a fix each time you use the unit. To insure trouble free operation, it is suggested that the battery be replaced every five years with an exact replacement lithium battery. Your authorized Raytheon distributor or Raytheon Factory Service Center can fit a replacement battery for you. 14 RAYSTAR 112 Installation and Operation Handbook 4.3 Trouble Shooting All Raytheon products undergo comprehensive testing prior to packaging and shipment from the factory. However, in the unlikely event that a problem arises, the following checks should help to locate the possible cause. Fault No data output after 30 min. operation. No satellites No fix No Data output Cause No DC power Action 1. Check power is switched on. 2. Check fuse/breaker 3. Verify antenna is not obstructed and is vertically mounted. 4. Check data connections for broken wires. Path blocked Chapter 4: Maintenance 15 4.4 Electrical Specifications: General: Receiver type: Frequency: Sensitivity: Signal Acquisition: Time to first fix: Maximum No. of tracked satellites: Almanac update: Accuracy (Typical): Position: Speed: Differential Correction: Geodetic Datum: Data Output: SA= Off SA= On +/- 15M +/- 100M 0.1 kts DGPS=On +/-5 to 8M 12 Channel, parallel, highspeed 1575.42 MHz +/- 1MHz (C/A code), L1 -130 dBm Automatic and computer controlled 10 minutes maximum; Less than 3 minutes after first fix. 12 Automatic Accepts RTCM SC-104 WGS-84 is default; 190 others programmable Single output port. NMEA 0183 includes RMC, GLL, VTG, GGA, GSA and GSV sentences. TTL level asynchronous serial data, 4800 baud. Via internal lithium battery, 3-5 years life 13.6 VDC, 0.25A nominal (11-16 VDC) Data Type: Memory Backup: Power Requirements: Mechanical Specifications: Antenna: Antenna Construction: Cable Type: Cable Length: Dimensions: Weight: Temperature: Storage Temperature: ADP Waterproof to USCG standard CFR 46 6 conductor, White PVC jacket 10 meters (33 ft) 110 x 130 mm (4.3" H x 5.1" W) 0.6 kg (1.3 lbs) approximately -20° to +70°C -40°C to +85° C 16 RAYSTAR 112 Installation and Operation Handbook Appendix 17 Appendix A Additional Local Geodetic Systems 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 Adindan (Mean for Ethiopia and Sudan) ARC 1950 (Mean for Botswana, Lesotho, Malawi, Swaziland, Zaire, Zambia, Zimbabwe) Australian Geodetic 1984 (Australia) Bermuda 1957 (Bermuda Islands) Bogota Observatory (Columbia) Campo Inchauspe (Argentina) Chatham 1971 (Chatham Island) Chua Astro (Paraquay) Corrego Alegre (Brazil) Djakarta (Vatavia) (Sumatra) European 1979 (Europe) Geodetic Datum 1949 (New Zealand) Guam 1963 (Guam) Hayford 1910 (Finland) Hjorsey 1955 (Iceland) Indian (India and Nepal) Ireland 1965 (Ireland) Kertau 1948 (West Malaysia and Singapore) L.C.5. Astro (Cayman Brac Island) Liberia 1964 (Liberia) Luzon (Philippines (excluding Mindanao)) Merchich (Morocco) Minna (Cameroon) Nahrwan (Oman) Naparima, BWI (Trinidad and Tobago) Old Egyptian (Egypt) Old Hawaiian (Hawaiian Islands) Pico De Las Nieves (Canary Islands) Provisional South American 1956 (Mean for Bolivia, Chile, Columbia, Ecuador, Guyana, Peru, Venezuela) Provisional South Chilean 1963 (Southern Chile) Puerto Rico (Puerto Rico and Virgin Islands) 18 RAYSTAR 112 Installation and Operation Handbook 42 43 44 45 Qornoq (Southern Greenland) RT90 (Sweden) Santa Braz (Sao Maguel and Santa Maria Islands) South American 1969 (Mean for Argentina, Bolivea, Brazil, Chile, Columbia, Ecuador, Guyana, Paraguay, Peru, Trinidad & Tobago, Venezuela) Southwest Base (Graciosa Base) (Faial, Graciosa, Pico, Sao Jorge and Terceira Island) Timbalai 1948 (Brunei and East Malaysia) Adindan (Burkina Faso) Adindan (Cameroon) Adindan (Ethiopia) Adindan (Mali) Adindan (Senegal) Adindan (Sudan) Afgooye (Somalia) Ain el Abd 1970 (Bahrain) Ain el Abd 1970 (Saudi Arabia) Ain el Abd 1970 (Cocos Islands) Antigua Island Astro 1943 (Antigua and Leeward Islands) Arc 1950 (Botswana) Arc 1950 (Burundi) Arc 1950 (Lesotho) Arc 1950 (Malawi) Arc 1950 (Swaziland) Arc 1950 (Zaire) Arc 1950 (Zambia) Arc 1950 (Zimbabwe) Arc 1950 (Mean for Kenya and Tanzania) Ascension Island 1958 (Ascension Island) Astro Beacon E 1945 (Iwo Jima) Astro DOS 71/4 (St Helena Island) Astro Tern Island 1961 (Tern Island) Astronomical Station 1952 (Marcus Island) Ayabelle Lighthouse (Djibouti) Bellevue (IGN) (Efate and Erromango Islands) 46 47 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 Appendix 19 77 78 79 80 81 82 83 84 85 86 87 88 89 90 91 92 93 94 95 96 97 98 99 100 101 102 103 104 105 106 107 108 Bissau (Guinea, Bissau) Bukit Rimpah (Indonesia (Bangka and Belitung Islands)) Camp Area Astro (Antarctica (McMurdo Camp)) Canton Astro 1966 (Phoenix Islands) Cape (South Africa) Cape Canaveral (Bahamas and Florida) Carthage (Tunisia) Dabola (Guinea) DOS 1968 (New Georgia Islands) Easter Island 1967 (Easter Island) European 1950 (Mean for Austria, Denmark, Germany, Netherlands, Switzerland) European 1950 (Mean for Iraq, Israel, Jordon, Lebanon, Kuwait, Saudi Arabia, Syria) European 1950 (Cyprus) European 1950 (Egypt) European 1950 (England, Channel Islands, Scotland, Shetland Islands) European 1950 (Finland, Norway) European 1950 (Greece) European 1950 (Iran) European 1950 (Italy (Sardinia)) European 1950 (Italy (Sicily)) European 1950 (Malta) European 1950 (Portugal ,Spain) European 1979 (Mean for Austria, Finland, Netherlands, Norway, Spain, Sweden, Switzerland) Fort Thomas 1955 (Nevis, St Kitts (Leeward Islands)) Gan 1970 (Maldives) Guam 1963 (Guam) Gunung Segara (Indonesia (Kalimantan)) GUX 1 Astro (Guadalcanal Island) Herat North (Afghanistan) Hong Kong 1963 (Hong Kong) Hu-Tzu-Shan (Taiwan) Indian (Bangladesh) 20 RAYSTAR 112 Installation and Operation Handbook 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 Indian 1954, (Thailand, Vietnam) Indian 1975 (Thailand) ISTS 061 Astro 1968 (South Georgia Islands) ISTS 073 Astro 1969 (Diego Garcia) Johnston Island 1961 (Johnston Island) Kandawala (Sri Lanka) Kerguelen Island 1949 (Kerguelen Island) Kusaie Astro 1951 (Caroline Islands) Legion Ghana Luzon Philippines (Philippines Mindanoa) Mahe 1971 (Mahe Island) Massawa (Ethiopia (Eritrea )) Midway Astro 1961 (Midway Island) Minna (Nigeria) Montserrat Island Astro 1958 (Montserrat (Leeward Islands)) M'Poraloko (Gabon) Nahrwan (Saudi Arabia) Nahrwan (United Arab Emirates) North American 1927 ( NAD27 ) (Mean for Antigua, Barbados, Barbuda, Caicos Islands, Cuba, Dominican Republic, Grand Cayman, Jamaica, Turks Islands) North American 1927 ( NAD27 ) (Mean for Belize, Costa Rica, El Salvador, Guatemala, Honduras, Nicaragua) North American 1927 ( NAD27 ) (Mean for CONUS ( East of Mississippi River)) North American 1927 ( NAD27 ) (MEAN for CONUS ( West of Mississippi River)) North American 1927 ( NAD27 ) (Alaska) North American 1927 ( NAD27 ) (Bahamas ( Except San Salvador Island)) North American 1927 ( NAD27 ) (Canada (Alberta, British Columbia)) North American 1927 ( NAD27 ) (Canada ( Manitoba, Ontario)) North American 1927 ( NAD27 ) (Canada (New Brunswick, Newfoundland, Nova Scotia, Quebec) North American 1927 ( NAD27 ) (Canada ( Northwest Territories, Saskatchewan)) 128 129 130 131 132 133 134 135 136 Appendix 21 137 138 139 140 141 142 143 144 145 146 147 148 149 150 151 152 153 154 155 156 157 158 159 160 161 162 163 164 165 166 167 168 169 North American 1927 ( NAD27 ) (Canada (Yukon)) North American 1927 ( NAD27 ) (Canal Zone) North American 1927 ( NAD27 ) (Cuba) North American 1927 ( NAD27 ) (Greenland (Hayes Peninsula)) North American 1927 ( NAD27 ) (Mexico) North American 1983 (Alaska, Canada, CONUS) North American 1983 (Central America, Mexico) Obersvatorio Metereo 1939 (Azores) Old Hawaiian (Mean for Hawaii, Kauai, Maui, Oahu) Old Hawaiian (Kauai) Old Hawaiian (Maui) Old Hawaiian (Oahu) Oman (Oman) Ordnance Survey of Great Britain 1936 (Mean for England, Isle of Man, Scotland, Shetland Islands , Wales) Ordnance Survey of Great Britain 1936 (England , Isle of Man, Wales) Ordnance Survey of Great Britain 1936 (Scotland, Shetland Islands) Ordnance Survey of Great Britain 1936 (Wales) Pitcairn Astro 1967 (Pitcairn Island) Point 58 (Mean for Burkina Faso and Niger) Pointe Noire 1948 (Congo) Porto Santo 1936 (Porto Santo, Madeira Islands) Provisional South American 1956 (Bolivia) Provisional South American 1956 (Chile (Northern Near 19°S )) Provisional South American 1956 (Chile ( Southern Near 43°S ) Provisional South American 1956 (Columbia) Provisional South American 1956 (Ecuador) Provisional South American 1956 (Guyana) Provisional South American 1956 (Peru) Provisional South American 1956 (Venezuela) Qatar National (Qatar) Reunion (Mascarene Islands) Rome 1940 (Italy, Sardinia) Santa(DOS) 1965 (Espirito Santo Island) 22 RAYSTAR 112 Installation and Operation Handbook 170 171 172 173 174 175 176 177 178 179 180 181 182 183 184 185 186 187 188 189 190 191 192 193 194 195 196 197 198 199 200 Sapper hill 1943 (East Falkland Island) Schwarzeck (Namibia) Selvagem Grande (Salvage Islands) SGS 85 Soviet Geodetic System 1985 (Russia) South American 1969 (Argentina) South American 1969 (Bolivia) South American 1969 (Brazil) South American 1969 (Chile) South American 1969 (Columbia) South American 1969 (Ecuador) South American 1969 (Ecuador (Baltra, Galapagos)) South American 1969 (Guyana) South American 1969 (Paraguay) South American 1969 (Peru) South American 1969 (Trinidad & Tobago) South American 1969 (Venezuela) South Asia (Singapore) Tananarive Observatory 1925 (Madagasar) Tokyo (Japan) Tokyo (Korea) Tokyo (Okinawa) Tristan Astro 1968 (Tristan de Cunha) Viti Levu 1916 (Fiji (Viti Levu Island)) Wake-Eniwetok 1960 (Marshall Islands) Wake Island Astro 1952 (Wake Atoll) Yacare (Uruguay) Zanderij (Suriname) Reserved Reserved Reserved User Defined 81126-1 Printed in England Document No. G623819-5 Raytheon Marine Company 676 Island Pond Road Manchester, NH 03109-5420 TEL (603) 647-7530 FAX (603) 634-4756 Raytheon Marine Europe Ltd. Anchorage Park, Portsmouth, Hampshire, PO3 5TD, England TEL (01705) 693611 FAX (01705) 694642