
Text extracted from the exhibit documents filed with the FCC. Open a document above to read the original.
- 1 - Space Data Corporation Confidential and proprietary information Space Data Corporation ® ________________________________________________________________________ Space Data Corporation SkySite System Operators Instructions Model SKS-900 SkySite Model GST-900 Ground Station Space Data Corporation 460 S Benson Lane Suite 11-12 Chandler, Arizona 85224-5663 March, 2004 - 2 - Space Data Corporation Confidential and proprietary information 1.0 Introduction. The Space Data Corporation SkySite network is designed to provide wireless paging service to remote areas that are not practically serviced by traditional terrestrial communication towers. This paging coverage is accomplished by mounting the functional equivalent of a communications tower on a high altitude weather balloon thereby overcoming service limitations. The SkySite Network consists of 5 subsystems listed below. 1. SkySite Platform 2. Launch Facilities 3. Ground Station 4. Network Control Center. 5. SkySite Control Center Wireless Data Carriers Wireless Voice Carriers Network Control Center - Carrier Gateways - Capacity Forecasting - Device Location - Network Management - ReFLEX - Mobitex - DataTac - GSM - CDMA - IDEN - TDMA SkySite™ Control Center - SkySite™ Location and Status - SkySite™ Antenna Tracking - SkySite™ Coverage Forecasting - SkySite™ Manual Commanding - Meteorological Data Processing WAN to Ground Stations Ground Stations - Transmitter - Receiver - Antenna - Antenna Controller SkySite™ Platforms - SkySite™ DSP - SkySite™ RF Circuitry - SkySite™ Control Processor - GPS Receiver - SkySite™ Vent - SkySite™ Ballast - SkySite™ Antenna Launch Facilities - SkySite™ Platforms - Supply of Lifting Gas - Weather Balloons Figure 1.1: The SkySite Network This document is a summary of the procedures used to deploy and operate the SkySite network. All equipment shown is manufactured, operated and serviced by Space Data Corporation and is therefore meant for internal use only. - 3 - Space Data Corporation Confidential and proprietary information 2.0 Launch Control Center operations are managed through the use of several Space Data Corp. proprietary software applications. These client applications run from EPS (Engineering Programming Software) server: GST (Ground Station). The GST maintains the communication link from the ground to the SkySite. The GST also monitors and controls ground station functions such as antenna auto-tracking, Receive signal strength, TX and RX power levels and frequency correction. SkySite client. Monitors SkySite performance such as TX and RX power levels, GPS position, battery current and voltage, and AH consumed. Vent ballast controls and accumulated values release command. Mapping client. This application utilizes the GPS coordinates sent from the SkySite and superimposes it on mapping software. Terrain and population density are easily determined from this screen and is used to plan recovery of the payload. 2.1 Pre-flight client preparation Start all GST (Ground Station Transceiver) and SKS (SkySite) clients. Both software applications should connect to the EPS (Engineering Programming Software) server. Determine the type of antenna used by the Ground station in operation. There are only two types of antennas used: 1. Omi-directional antenna (Max. Gain of 3dBi) 2. Yagi antenna (Max. Gain of 10dBi) Caution: In order to comply with FCC Part 24 and RF (Radio Frequency) exposure limits of this product the maximum GST ERP (Effective Radiated Power) must not exceed 7 Watts (38.45dBm). Transmit power levels are shown in the bottom left corner of the GST client in the “TX GLP HPA STATUS” box. This value does not include the directional gain of the antenna. Therefore the maximum permissible power levels into the antenna as are as follows: 1. Using the Omni-directional antenna the maximum power is 35dBm. 2. Using the high gain Yagi antenna the maximum power is 28dBm. - 4 - Space Data Corporation Confidential and proprietary information • Start all GST and SKS clients. Ensure that GST clients connect to EPS server. On GST Client open the GLP RSSI and GPS screens • On the SKS Client open the following screens: GPS. GLP RSSI. Altitude vs. heading graphs. Altitude vs. Horizontal speed. Vertical speed graph. • Check Antenna Control: Disable tracking Ensure client is in “remote tracking” mode. For each GST client slew antenna in azimuth and elevation. Point antenna toward launch site at 0 degrees elevation. • Start GPS client on mapping PC and ensure it connects to EPS server. The GPS client started must correspond to the GST that will be used to control the payload. • Start predictor software on mapping PC • Start Delorme payload and predictor programs on mapping PC. 2.2 Launch procedure: • Switch GST client to launch frequency • Watch RSSI level. When Rx Sync has indicator turn green call launch team and give them the OK to release the SkySite. • When SkySite is picked up by the GST and signal is stable call launch team and have them go to listen mode. • When you see the RSSI signal level drop on the SkySite enter command mode on GST. • Confirm auto hover is engaged and set for the correct altitude • Switch SkySite to operational frequency at high power: • On configuration screen select an operational frequency, select “non-volatile” and click set. • On the GST client go to the configuration screen and switch it’s frequency to the one that the SkySite is using and re-acquire the SkySite. • On the SkySite client go to the “configuration” screen and select an output power of 33 dB. Select “non-volatile” and click set. • Reduce the power of the SkySite to the minimum power required. Ensure that it is a “volatile” change. • Confirm that ReFLEX is enabled. - 5 - Space Data Corporation Confidential and proprietary information 3.0 Flight termination • When the useful life of the SkySite, turn command over to the recovery team and let them know the SkySite will be switching over to a recovery frequency. • Switch SkySite…
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Ground Station Photographs GST Front View GST-900 Rear View GST-900 Top View GST-900 Bottom View GST-900 Right Side View GST-900 Left Side View
FCC Label Location and Compliance Statement An FCC identification and compliance label is affixed to the GST chassis, next to the RF output connector. Space Data corporation’s grantee code “RY9” is displayed with the Ground Station model number as FCC ID “RY9GST900” as shown in the figures below. FCC ID: RY9GST900 Model: GST-900 This device complies with Part 15 of the FCC Rules. Operation is subject to the following two conditions: 1) This device may not cause harmful interference and 2) This device must accept any interference that may be received, including interference that may cause undesired operation.' Made in U.S.A. FCC Label Graphics FCC Label Location Space Data Corporation ®
Ground Station Printed Circuit Identification and Photographs. Printed Circuit Identification High Intercept Receiver AS1043 Flight Computer AS1003 Baseband Test Board AS1006 Baseband Board AS1004 Transceiver Board AS1005 COTS Power Supply Baseband Test Board, Front View Baseband Test Board, Rear View Flight Computer, Front View Flight Computer, Rear View with COTS GPS Receiver (Motorola M-12) Flight Computer, Rear View Tranciever, Front View Tranciever, Rear View Basband Board, Front View Baseband Board, Rear View High Intercept Board, Front View High Intercept Board, Rear View
Environmental Assessment for Mobiles/Fixed Base Station for FCC ID: FCC ID: RY9GST900 Model:GST-900 to Federal Communications Commission 47 CFR 1.1310 (MPE) Radiofrequency Radiation Exposure Limits Date Of Report: April 6, 2004 On the Behalf of the Applicant: Space Data Corporation At the Request of: P.O. 20610 Space Data Corporation 460 S. Benson Lane, Suite 11-12 Chandler, AZ 85224 Attention of: Gerard J. Quenneville, Vice President Engineering (480) 722-2100; FAX: (480) 403-0021 [email protected] Bill McCullough Supervised By: Morton Flom, P. Eng. Table of Contents Rule Description Page . Test Report 1 . Identification of the Equipment Under Test 2 . Standard Test Conditions and Engineering Practices 4 1.1310 Environmental Assessment 5 Page Number 1 of 8. Required information per ISO/IEC Guide 25-1990, paragraph 13.2: a) Test Report (Supplemental) b) Laboratory: (FCC: 31040/SIT) (Canada: IC 2044) M. Flom Associates, Inc. 3356 N. San Marcos Place, Suite 107 Chandler, AZ 85225 c) Report Number: d0440019 d) Client: Space Data Corporation 460 S. Benson Lane, Suite 11-12 Chandler, AZ 85224 e) Identification: GST-900 FCC ID: RY9GST900 Description: Base Station f) EUT Condition: Not required unless specified in individual tests. g) Report Date: April 6, 2004 EUT Received: March 22, 2004 h, j, k): As indicated in individual tests. i) Sampling method: No sampling procedure used. l) Uncertainty: In accordance with MFA internal quality manual. m) Supervised by: Morton Flom, P. Eng. n) Results: The results presented in this report relate only to the item tested. o) Reproduction: This report must not be reproduced, except in full, without written permission from this laboratory. Page Number 2 of 8. Identification of the Equipment Under Test (EUT) Name and Address of Applicant: Space Data Corporation 460 S. Benson Lane, Suite 11-12 Chandler, AZ 85224 Manufacturer: Applicant FCC ID: RY9GST900 Model Number: GST-900 Description: Ground Station Type of Emission: 10K0F1D Frequency Range, MHz: 901 to 902 Power Rating, Watts: 7.0 Switchable X Variable N/A Modulation: AMPS TDMA CDMA X OTHER Antenna: Helical Monopole X Whip X Other Note: For RF Safety test antenna gain taken at the upper range of expected gain (i.e. 0 dBd) and RF Power set to highest nominal power across all channels. Page Number 3 of 8. NIST Page Number 4 of 8. Standard Test Conditions and Engineering Practices Except as noted herein, the following conditions and procedures were observed during the testing: In accordance with ANSI C63.4-1992/2000, section 6.1.9, and unless otherwise indicated in the specific measurement results, the ambient temperature of the actual EUT was maintained within the range of 10° to 40°C (50° to 104 °F) unless the particular equipment requirements specify testing over a different temperature range. Also, unless otherwise indicated, the humidity levels were in the range of 10% to 90% relative humidity. Prior to testing, the EUT was tuned up in accordance with the manufacturer's alignment procedures. All external gain controls were maintained at the position of maximum and/or optimum gain throughout the testing. Measurement results, unless otherwise noted, are worst-case measurements. Page Number 5 of 8. Name of Test: Environmental Assessment Specification: FCC: 47 CFR 1.1310 Measurement Guide: ANSI/IEEE C95.1 1992 Test Equipment: Maximum Permissible Exposure (MPE) measurement system, consisting of: Narda 8717-1174R, Radiation meter Narda 8761D, E-field probe (300 kHz – 3 GHz) (Calibrated Feb-2003) Measurement Procedure: 1. The following measurements were performed with a Narda probe using ANSI/IEEE C95.1 as a guide. 2. Prior to making any measurements, the measurements system was calibrated in accordance with the manufacturer’s procedures. 3. The EUT’s radiating element (antenna) was placed on a 1 m tall table for ease of testing. For equipment normally operated on a metal surface, a ground plane was used. 4. The remaining equipment necessary to operate the EUT was maintained at a distance from the measurement arrangement suitable to minimize interference with the measurements. 5. The minimum safe distance was calculated from the formula Power Density = EIRP / 4πR 2 (Peak Watts/m 2 ). The calculation is shown with the measurement data. 6. With the EUT operating at maximum power, a search was initiated for worst case emissions with the probe raised and lowered over a range of 0.2 to 2 meters in height and over a horizontal plane of 0 o to 360 o . 7. Average values were calculated for the whole body (0.2- 2.0m), lower body (0.2-0.8m) and upper body (1.0-2.0m). Results: Attached. Page Number 6 of 8. Test Setup: Maximum Permissible Exposure (MPE) Whip Yagi Page Number 7 of 8. Name of Test: R.F. Radiation Exposure FCC Rules: 1.1307, 1.1310, 1.1311, 2.1091 Description, EUT: See page 2 of Test Report Test Frequency, MHz = 901.475 Antenna Gain = 3 dBi Omni Antenna Model ¼ Wave X ⅝ Wave Other dBd Other 0.3-1.234 MHz: Limit [mW/cm 2 ] = 100 1.34-30 MHz: Limit [mW/cm 2 ] = (180/f 2 ) 30-300 MHz: Limit [mW/cm 2 ] = 0.2 Limits: Uncontrolled Exposure 47 CFR 1.1310 Table 1, (B) 300-1500 MHz Limit [ mW/cm 2 ] = f/1500 1500-100,000 MHz: Limit [ mW/cm 2 ] = 1.0 Power [W EIRP] = P [conducted] x G [antenna] = 7W Limit [mW/cm2] = 0.600 Limit [W/m2] = 10 x Limit [mW/cm2] = 6.00 R [m] = [P [W EIRP] / (4π x Limit [W/m2] )] 1/2 = 0.293 Pre-test Calculations Probe Height, m Power Density, mW/cm 2 2.0 0.10 1.8 0.15 1.6 0.19 1.4 0.21 1.2 0.25 1.0 0.24 0.8 0.20 0.6 0.17 0.4 0.12 Results: at tested distance 50cm 0.2 0.10 Power Density Calculations: The measured power density readings were summed and the results divided by the number of readings to calculate the average. For whole body: Average of 0.2 to 2.0 m, mW/cm 2 = 0.173 For lower body: Average of 0.2 to 0.8 m, mW/cm 2 = 0.148 For upper body: Average of 1.0 to 2.0 m, mW/cm 2 = 0.190 Supervised By: Morton Flom, P. Eng. Page Number 8 of 8. Name of Test: R.F. Radiation Exposure FCC Rule…
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Page Number 7 of 8. Amended April 12, 2004 Name of Test: R.F. Radiation Exposure FCC Rules: 1.1307, 1.1310, 1.1311, 2.1091 Description, EUT: See page 2 of Test Report Test Frequency, MHz = 901.475 Antenna Gain = 3 dBi Omni Antenna Model ¼ Wave X ⅝ Wave Other dBd Other 0.3-1.234 MHz: Limit [mW/cm 2 ] = 100 1.34-30 MHz: Limit [mW/cm 2 ] = (180/f 2 ) 30-300 MHz: Limit [mW/cm 2 ] = 0.2 Limits: Uncontrolled Exposure 47 CFR 1.1310 Table 1, (B) 300-1500 MHz Limit [ mW/cm 2 ] = f/1500 1500-100,000 MHz: Limit [ mW/cm 2 ] = 1.0 Power [W EIRP] = P [conducted] x G [antenna] = 7W Limit [mW/cm2] = 0.600 Limit [W/m2] = 10 x Limit [mW/cm2] = 6.00 R [m] = [P [W EIRP] / (4π x Limit [W/m2] )] 1/2 = 0.293 Pre-test Calculations Probe Height, m Power Density, mW/cm 2 2.0 0.230 1.8 0.345 1.6 0.437 1.4 0.483 1.2 0.575 1.0 0.552 0.8 0.460 0.6 0.391 0.4 0.276 Results: at tested distance 30cm 0.2 0.230 Power Density Calculations: The measured power density readings were summed and the results divided by the number of readings to calculate the average. For whole body: Average of 0.2 to 2.0 m, mW/cm 2 = 0.398 For lower body: Average of 0.2 to 0.8 m, mW/cm 2 = 0.339 For upper body: Average of 1.0 to 2.0 m, mW/cm 2 = 0.437 Supervised By: Morton Flom, P. Eng. Page Number 8 of 8. Amended April 12, 2004 Name of Test: R.F. Radiation Exposure FCC Rules: 1.1307, 1.1310, 1.1311, 2.1091 Description, EUT: See page 2 of Test Report Test Frequency, MHz = 901.475 Antenna Gain = 10 dBi Yagi Antenna Model ¼ Wave ⅝ Wave Other dBd 7.85 Other 0.3-1.234 MHz: Limit [mW/cm 2 ] = 100 1.34-30 MHz: Limit [mW/cm 2 ] = (180/f 2 ) 30-300 MHz: Limit [mW/cm 2 ] = 0.2 Limits: Uncontrolled Exposure 47 CFR 1.1310 Table 1, (B) 300-1500 MHz Limit [ mW/cm 2 ] = f/1500 1500-100,000 MHz: Limit [ mW/cm 2 ] = 1.0 Power [W EIRP] = P [conducted] x G [antenna] = 7W Limit [mW/cm2] = 0.600 Limit [W/m2] = 10 x Limit [mW/cm2] = 6.00 R [m] = [P [W EIRP] / (4π x Limit [W/m2] )] 1/2 = 0.293 Pre-test Calculations Probe Height, m Power Density, mW/cm 2 2.0 0.046 1.8 0.184 1.6 0.299 1.4 0.437 1.2 0.529 1.0 0.552 0.8 0.437 0.6 0.345 0.4 0.207 Results: at tested distance 30cm 0.2 0.138 Power Density Calculations: The measured power density readings were summed and the results divided by the number of readings to calculate the average. For whole body: Average of 0.2 to 2.0 m, mW/cm 2 = 0.317 For lower body: Average of 0.2 to 0.8 m, mW/cm 2 = 0.282 For upper body: Average of 1.0 to 2.0 m, mW/cm 2 = 0.341 Supervised By: Morton Flom, P. Eng. (The following will be placed in the Instruction Manual) Mandatory Safety Instructions to Installers & Users Use only manufacturer or dealer supplied antenna. Antenna Minimum Safe Distance: 30cm. Antenna Gains: Three dBi on High Power with whip (+0.85dB referenced to a dipole) and ten dBi on Low Power with Yagi (+7.85dB referenced to a dipole). Rule Part 24D limit is 7W ERP The Federal Communications Commission has adopted a safety standard for human exposure to RF (Radio Frequency) energy which is below the OSHA (Occupational Safety and Health Act) limits. Antenna Mounting: The antenna supplied by the manufacturer or radio dealer must not be mounted at a location such that during radio transmission, any person or persons can come closer than the above indicated minimum safe distance to the antenna i.e. 30cm To comply with current FCC RF Exposure limits, the antenna must be installed at or exceeding the minimum safe distance shown above, and in accordance with the requirements of the antenna manufacturer or supplier. Base Station Installation: The antenna should be fixed-mounted on an outdoor permanent structure. RF Exposure compliance must be addressed at the time of installation. Antenna Substitution: Do not substitute any antenna for the one supplied or recommended by the manufacturer or radio dealer. You may be exposing person or persons to excess radio frequency radiation. You may contact your radio dealer or the manufacturer for further instructions. Warning: Maintain a separation distance from the antenna to a person(s) of at least 30cm. You, as the qualified end-user of this radio device must control the exposure conditions of bystanders to ensure the minimum separation distance (above) is maintained between the antenna and nearby persons for satisfying RF Exposure compliance. The operation of this transmitter must satisfy the requirements of Occupational/Controlled Exposure Environment, for work-related use. Transmit only when person(s) are at least the minimum distance from the properly installed, externally mounted antenna.
FCC ID: RY9GST900 Transmitter Certification of FCC ID: RY9GST900 Model: GST-900 to Federal Communications Commission Rule Part(s) 24D, Confidentiality Date of report: April 6, 2004 On the Behalf of the Applicant: Space Data Corporation At the Request of: P.O. 20610 Space Data Corporation 460 S. Benson Lane, Suite 11-12 Chandler, AZ 85224 Attention of: Gerard J. Quenneville, Vice President Engineering (480) 722-2100; FAX: (480) 403-0021 [email protected] Bill McCullough Supervised by: Morton Flom, P. Eng. MFA p0430010, d0440008 FCC ID: RY9GST900 List of Exhibits (FCC Certification (Transmitters) - Revised 9/28/98) Applicant: Space Data Corporation FCC ID: RY9GST900 By Applicant: 1. Letter of Authorization x 2. Confidentiality Request: 0.457 And 0.459 x 4. Identification Drawings, 2.1033(c)(11) x Label x Location of Label x Compliance Statement x Location of Compliance Statement 5. Photographs, 2.1033(c)(12) x 6. Documentation: 2.1033(c) (3) User Manual x (9) Tune Up Info x (10) Schematic Diagram x (10) Circuit Description x Block Diagram x Active Devices x 7. MPE Report x By M.F.A. Inc.: A. Testimonial & Statement of Certification MFA p0430010, d0440008 FCC ID: RY9GST900 The Applicant has been cautioned as to the following: 15.21 Information to the User. The users manual or instruction manual for an intentional radiator shall caution the user that changes or modifications not expressly approved by the party responsible for compliance could void the user's authority to operate the equipment. 15.27(a) Special Accessories. Equipment marketed to a consumer must be capable of complying with the necessary regulations in the configuration in which the equipment is marketed. Where special accessories, such as shielded cables and/or special connectors are required to enable an unintentional or intentional radiator to comply with the emission limits in this part, the equipment must be marketed with, i.e. shipped and sold with, those special accessories. However, in lieu of shipping or packaging the special accessories with the unintentional or intentional radiator, the responsible party may employ other methods of ensuring that the special accessories are provided to the consumer, without additional charge. Information detailing any alternative method used to supply the special accessories for a grant of equipment authorization or retained in the verification records, as appropriate. The party responsible for the equipment, as detailed in § 2.909 of this chapter, shall ensure that these special accessories are provided with the equipment. The instruction manual for such devices shall include appropriate instructions on the first page of text concerned with the installation of the device that these special accessories must be used with the device. It is the responsibility of the user to use the needed special accessories supplied with the equipment. MFA p0430010, d0440008 FCC ID: RY9GST900 Table of Contents Rule Description Page . Test Report 1 2.1033(c) General Information Required 2 2.1033(c)(14) Rule Summary 5 . Standard Test Conditions and Engineering Practices 6 2.1046(a) Carrier Output Power (Conducted) 7 2.1046(a) ERP Carrier Power (Radiated) 9 2.1053(a) Field Strength of Spurious Radiation 12 2.1049(c)(1) Emission Masks (Occupied Bandwidth) 16 2.1055(a)(1) Frequency Stability (Temperature Variation) 24 2.1055(b)(1) Frequency Stability (Voltage Variation) 27 2.202(g) Necessary Bandwidth and Emission Bandwidth 27 MFA p0430010, d0440008 FCC ID: RY9GST900 Page Number 1 of 27. Required information per ISO/IEC Guide 25-1990, paragraph 13.2: a) Test Report b) Laboratory: (FCC: 31040/SIT) (Canada: IC 2044) M. Flom Associates, Inc. 3356 N. San Marcos Place, Suite 107 Chandler, AZ 85225 c) Report Number: d0440008 d) Client: Space Data Corporation 460 S. Benson Lane, Suite 11-12 Chandler, AZ 85224 e) Identification: GST-900 FCC ID: RY9GST900 EUT Description: Base Station f) EUT Condition: Not required unless specified in individual tests. g) Report Date: April 6, 2004 EUT Received: March 22, 2004 h, j, k): As indicated in individual tests. i) Sampling method: No sampling procedure used. l) Uncertainty: In accordance with MFA internal quality manual. m) Supervised by: Morton Flom, P. Eng. n) Results: The results presented in this report relate only to the item tested. o) Reproduction: This report must not be reproduced, except in full, without written permission from this laboratory. MFA p0430010, d0440008 FCC ID: RY9GST900 Page Number 2 of 27. List of General Information Required for Certification In Accordance with FCC Rules and Regulations, Volume II, Part 2 and to 24D, Confidentiality Sub-part 2.1033 (c)(1): Name and Address of Applicant: Space Data Corporation 460 S. Benson Lane, Suite 11-12 Chandler, AZ 85224 Manufacturer: Applicant (c)(2): FCC ID: RY9GST900 Model Number: GST-900 (c)(3): Instruction Manual(s): Please see attached exhibits (c)(4): Type of Emission: 10K0F1D (c)(5): Frequency Range, MHz: 901 to 902 (c)(6): Power Rating, Watts: 7.0 ERP Switchable X Variable N/A FCC Grant Note: BE - The output power is continuously variable from the value listed in this entry to 15%- 20% of the value listed. (c)(7): Maximum Power Rating, Watts: 7.0 (Defined as mobile per FCC MOO DA01-2132 dtd September 12, 2001) DUT Results: Passes x Fails MFA p0430010, d0440008 FCC ID: RY9GST900 Page Number 3 of 27. NIST MFA p0430010, d0440008 FCC ID: RY9GST900 Page Number 4 of 27. Subpart 2.1033 (continued) (c)(8): Voltages & currents in all elements in final RF stage, including final transistor or solid-state device: Collector Current, A = per manual Collector Voltage, Vdc = per manual Supply Voltage, Vdc = 115 vac (c)(9): Tune-Up Procedure: Please see attached exhibits (c)(10): Circuit Diagram/Circuit Description: Including description of circuitry & devices provided for determining and stabilizing frequency, for suppression of spurious radiation, for limiting modulation and limiting power. Please see attached e…
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| # | Rule Parts | Frequency Range | Power Output | Emission | Tolerance |
|---|---|---|---|---|---|
| 1 | 24D | 901 MHz - 902 MHz | 7 W | 10K0F1D | 1.0000000000 ppm |

Narrowband PCS, Multi-Protocol SkySite
Equipment Class
PCB - PCS Licensed Transmitter
SkySite Voice Repeater
Equipment Class
AMP - Amplifier
Narrow Band PCS
Equipment Class
PCB - PCS Licensed Transmitter