Description

1009-EX-CN-2018 Text Documents

Raytheon SAS

2018-12-17ELS_221303

Raytheon Multi-Program Testbed GPS Re-Radiator Justification Ontario California International Airport, Fixed Installation 1. Individual authorization is necessary for each device at a specific location. Noted. Raytheon is only requesting a single unit at the fixed location specified by 1923 East Avion Street Ontario, CA, Ontario International Airport California, N 34 deg 03' 08", W 117 deg 36' 40" 2. Applications for frequency assignment should be applied for as an XT station with a note indicating the device is to be used as an "Experimental RNSS Test Equipment for the purpose of testing GPS receivers". Noted. Raytheon Space & Airborne Systems is requesting permission to install and operate a Global Positioning System (GPS) re-radiator at our new Ontario International Airport California, hangar facility. The GPS re-radiator receives normal free-space GPS RF signals and repeat transmits them into the hangar facility interior. The GPS re-radiator will be utilized to support the Raytheon Multi-Program Testbed (RMT) aircraft. The RMT aircraft is a testbed developed to support avionics programs. The RMT aircraft is normally positioned within the hangar during ground operations and pre-flight activities. The GPS re-radiator will provide the normal GPS signals into the hangar interior thus simulating an out-of-hangar GPS RF environment. This will save the RMT program time and effort by eliminating the requirement to position the aircraft out of the hangar during these frequently scheduled program activities. 3. Approved applications for frequency assignment will be entered in the GMF Noted. 4. The maximum length of the assignment will be two years, with possible renewal. 1

The RMT program currently anticipates a program need of the STA for 6 months until the move is complete and our government contract is renewed. 5. The operation must be at specified location and mobile operation is not authorized. Raytheon Space and Airborne Systems is only requesting a single unit at the fixed location specified by: 1923 East Avion Street Ontario, CA, Ontario International Airport California, N 34 deg 03' 08", W 117 deg 36' 40" 6. The area of potential interference to GPS reception (e.g., military or contractor facility) has to be under the control of the user. The area of potential interference is contained within leased hangar and tarmac space controlled by Raytheon Space and Airborne Systems. 7. The maximum equivalent isotropically radiated power must be such that the emissions are no greater than -140 dBm/24 MHz at a distance of 100 feet (30 meters) from the building where the test is being conducted. The calculations showing compliance with this requirement must be provided with the application for frequency assignment and should be based on free space propagation with no allowance for building attenuation. Refer to attachments #1 and 2. 8. GPS users in the area of potential interference to GPS reception must be notified that GPS information may be impacted for periods of time. The only user of GPS information within the area of potential interference is the requesting organization, Raytheon Space and Airborne Systems. All Raytheon Space and Airborne Systems personnel or supporting contractors will be notified of the availability and use of the requested GPS re-radiation system within the area of potential interference. 9. The use is limited to activity for the purpose of testing RNSS equipment/systems. The application and use of the requested unit is solely for the support of testing RNSS equipment or systems. 2

Raytheon Space & Airborne Systems is requesting permission to install and operate a Global Positioning System (GPS) re-radiator at the program's Ontario CA International Airport hangar facility. The GPS re-radiator receives normal free-space GPS RF signals and repeat transmits them into the hangar facility interior. The GPS re-radiator will be utilized to support the RMT aircraft. The RMT aircraft is a testbed developed to support avionics programs. The RMT aircraft is normally positioned within the hangar during ground operations and pre-flight activities. The GPS re-radiator will provide the normal GPS signals into the hangar interior thus simulating an out-of-hangar GPS RF environment. This will save the RMT program time and effort by eliminating the requirement to position the aircraft out of the hangar during these frequently scheduled program activities. 10. A "Stop Buzzer" point of contact for the authorized device must be identified and available at all times during GPS re-radiation operation of the device under any condition. (Rev. 9/2005) Mr. Alan Wigdahl 310-417-3706, is the supervisor of the facility where the GPS re- radiator will be located. The backup individual for this purpose is Mr. John Mallet, 310-417-3714. The input power to the GPS re-radiation unit is controlled by a single power subpanel circuit breaker located adjacent to the Raytheon Space and Airborne Systems maintenance office. The circuit breaker is clearly labeled and under the direct control of Mr. Gerome at all times. 3

ATTACHMENT #1 GPS Reradiation Signal Strength Specifications and Evaluation Below is the computation of the signal level, as transmitted by the reradiation kit, at a fixed distance from the repeater antenna. In particular we are interested in the computed signal level at a distance of 100 ft. from the hangar door. Calculation: Signal level of GPS in open space (from the satellites) received at the antenna. -158.5 dBW (L1 Frequency) -164.5 dBW (L2 Frequency) LNA amplifier gain in the receive antenna + 38 dB Signal loss through 75 feet of coaxial cable (LMR-400 specified at 6dB of loss per 100 ft.) - 4.5 dB Reradiation Amplifier gain + 20 dB__ Computed L1 Signal Output at the reradiation antenna - 105.0 dBW Computed L2 Signal Output at the reradiation antenna - 111.0 dBW Signal Loss Through Space: A sharp attenuation of the GPS signal occurs in the first 10 feet away from the reradiation antenna with a loss of approximately 50dB at that distance. At 50 feet, the expected loss would be 60dB. At 100 feet the signal attenuates by about 65dB from the starting level at the reradiation antenna. Computed L1 signal level at antenna - 105.0 dBW Computed L2 signal level at antenna - 111.0 dBW Signal loss through space at 100 feet - 65dB Therefore, Frequency L1 Signal level at 100 feet -170.0 dBW or -140.0 dBm Frequency L2 Signal level at 100 feet -176.0 dBW or -146.0 dBm 4

ATTACHMENT #2 GPS Reradiation Signal Pattern N 56 ft. R 60 ft. 3dB L2 Circle CL Note: 3dB L1 Circle is beyond Hangar doors shown closed the dimensions of this diagram. 5

GPSNetworkingInc. LA20RPDC Technical Product Data Features • Amplifier Gain of 20dB Gain ≥ 20dB • Extremely Flat Group Delay Less than 1ns Variation • Excellent Gain Flatness Gain | L1 - L2 | < 1.0 dB Description The LA20RPDC GPS Line Amplifier is a one input, one output device with a 20dB min. gain block. The frequency response covers the GPS L1 & L2 bands with excellent flatness. In the normal configuration, the RF output (J1) passes DC from the connected GPS receiver through the amplifier to the antenna, allowing the GPS receiver to power both the antenna and the amp. 0 Electrical Specifications, TA = 25 C Parameter Conditions Min Typ Max Units Freq. Range Ant – J1 1.1 1.7 GHz In/Out Imped. (1) Ant, J1 50 Ω Gain Ant – J1 20 24.5 26 dB Input SWR J1 - 50Ω 1.8:1 - Output SWR Ant - 50Ω 1.8:1 - Noise Figure Ant – J1 3.3 3.5 dB Gain Flatness | L1 - L2 |, Ant – J1 0.5 1 dB Reverse Isolation J1 – Ant 35 dB Group Delay τd,max - τd,min : Ant – J1 1 ns Flatness Req. DC Input V. Non-Network Configuration, DC Input on J1 3.6 15 Vdc Current (2) Amplifier Current Draw, All prots - 50Ω 15 mA (1). Input/Output Impedance = 75Ω for 75Ω connector option. (2). Current draw on J1 port in the non-networked configuration. REV. A 11/10/04 1

Available Options Network Power Supply Source Voltage Options VOLTAGE INPUT STYLE 110VAC Transformer (Wall Mount) 220 VAC Transformer (Wall Mount) 240 VAC (United Kingdom) Transformer (Wall Mount) Customer Supplied DC 8-28 VDC Military Style Connector Output Voltage Options (1) DC VOLTAGE OUT MAX CURRENT OUT FOR CORRESPONDING Vout(2) 5V 110mA 7.5V 130mA 9V 140mA 12V 170mA 15V 210mA Custom TDB Pass/Block DC Options Pass DC(1) All Ports Pass DC DC Blocked (1) Ant is DC blocked, Pass DC J1 RF Connector Options Connector Options CONNECTOR STYLE CHARGE Type N NC Type SMA NC Type TNC NC Type N - 75Ω Contact Sales Agent (1). With Network Option, any RF port (input or output) can be DC blocked or can pass the network DC voltage. (2). TA = +50oC. Assuming Source of 110V, 220 or 240V Wall Mount Transformer. In general, maximum output current can be determined by: Iout ≤ 2.9 / (VsourceDC – Vout) A Part Number N LA20F PDC - S / 5 / 110 Network Option: N =Network Opt. ; Blank: No Network DC Options: DCB: Ant. DC Blocked ; PDC: Pass DC. Connector Options: N: N type; S: SMA; T: TNC; N75: N type -75Ω DC Output Voltage: 5, 7.5, 9, 12, 15, CXX (Custom:“XX” denotes the desired V) Source Voltage: 110 -Transformer, 220 – Transformer, 240 – Transformer, MC – Military Conn. (User supplies DV Voltage) REV. A 11/10/04 2

Performance Input SWR (Ant. Port) and Frequency Response: Ant. To J1 (Typical, type N conn.): Mechanical Dimensions: Height: 1.3” Length (not including connectors) Body: 2.5” Base Plate: 3.25” Width: 2.5” Weight: 10 oz. (286 grams) Operating Temp. Range: -40o to + 75oC REV. A 11/10/04 3

GPS L1 Antenna Active Page 1 of 1 L1 Antennas Performance Specifications: Part Number: L1ACE Frequency Range: 1575.42+-5MHz VSWR: 2.5:1 (max.) Amplifier Gain: 38dB (min.) Noise Figure: 1.5dB (max.) Voltage: 4.5 to 5.5 VDC Polarization: Right-Hand Circular Impedance: 50 Ohms Temperature: -40 to +80 C Connector: TNC, Female Performance Specifications: Part Number: L1ANTC Frequency L1: (1575.42+-10) MHz VSWR: 1.5:1 DC Grounding: Yes (lightening protection) LNA Noise Figure: less than 2.4dB LNA Gain: 33.0+-3.0dB LNA Current Draw: less than 30mA LNA Votlage: +3.5 to +24VDC Rejection: 2 2-Pole Filters Part Number: L1ARINC Polarization: Right-Hand Circular Impedance: 50 Ohms Temperature: -55 to +85 C Connector: SMA, Female Design Specifications: FAA TSO-C144 DO-160D, D0-228 MIL-C-5541, MIL-E-5400 MIL-I-45208A, MIL-STD-810 Toll Free: 866-289-4777 Telephone: 719-561-9520 Fax: 719-565-0890 sales@gpssource.com HOME | COMPANY INFORMATION | GPS SERVICES | PRODUCTS | FAQ | DISTRIBUTOR | GPS LINKS http://www.gpssource.com/htdocs/l1ant.html 8/8/2005

A11 in line GPS L1/L2 GLONASS Amplifier Product Data Page 1 of 2 A11 Product Data PRODUCTS | A11 http://www.gpssource.com/htdocs/a11data.html 8/8/2005

A11 in line GPS L1/L2 GLONASS Amplifier Product Data Page 2 of 2 Electrical Specifications: Mechanical Specifications: Frequency response for GPS L1/L2 and GLONASS 1GHz to 2GHz Dimension Flatness less than 3.5dB Length 2.5" Noise figure less than 1.8dB Width 2.5" Height 1.25" All ports can either pass DC or block DC voltage Base Plate 3.25"x2.5" 30dB gain 50 ohm impedance on both ports Operating Temperature Input & Output SWR less than 2.0:1 -40 to 75 degrees C Reverse Isolation greater than 49dB Required DC input 3.1 to 15VDC Current draw less than 14mA @ 3V DC input http://www.gpssource.com/htdocs/a11data.html 8/8/2005

L1 GPS Antenna Passive Page 1 of 1 L1 Passive Antennas Part Number: L1P2 Performance Specifications: Frequency: 1.575 GHz VSWR: 1.5:1 Bandwidth: 20Mhz (min.) Peak Gain: 3 dBic (min.) Polarization: Right-Hand Circular Impedance: 50 Ohms Temperature: -40 to +85 C Connector: SMA, Female Toll Free: 866-289-4777 Telephone: 719-561-9520 Fax: 719-565-0890 sales@gpssource.com HOME | COMPANY INFORMATION | GPS SERVICES | PRODUCTS | FAQ | DISTRIBUTOR | GPS LINKS http://www.gpssource.com/htdocs/l1pant.html 8/8/2005

adeg I0 S0 S0 uer SPECIFICATIONS ELECTRICAL: EREQUENCY: Lt: (1575.42 412) MHz ] 1.2; (1227.60 +12) MHz RADIATION PATTERN: HEMISPHERICAL ] I POLARIZATION: RHCP RHCP D .950 [24.13] VSWR: <1.5:1 <1.511 > IMPEDANCE: 50 ohms 50 ohms 1.900 [48.26] . ! q »3.500 [88.90] ANTENNA GAIN (dBic): Free Space 4R G.P. |FreeSpace <| 4R GP. @ 90 " (ZENITH): + 4.7 +3.5 + 3.3 +4.9 10 ° Elevation: ~1.8 ~ —2.0 —3.8 ~36 @ 20 " Clevation: ~0.3 +0.8 —2.0 —0.1 @ 30 * Efevation: + 1.4 + 1.8 —0.5 — 1.8 _@50— 20 * Elevation: >3.9 > 28 > 2.7 >3.0 _ | BEAM WIDTH (30B): 114 Deg. 139 Deg. 106 Deg. 75 Deg. AXIAL RATIO: 24B . 2dB 4X #,20 [0§.11] Thru. LIGHTNING PROTECTION: DC GROUNDING #.385 (#9.78] x 100 i LNA GAIN: 33 dB 35 dB for 10—32 MOUNTING SCREWS | LNA NOISE FIQURE: 3.0 48 3.0 dB 950 (24.13]) —— | LNA P1dB Out: LNA DC POWER: +13 dBm 2.5VIZOmA, gVIRDMA, 3.3V/3G5MmA, (2.5—24)V/<50mA +13 dBm w 1.900 [48.25) |r.. . REJECTION @(—50/+50) MHz —41 dB / —59 dB ] ~40 08 / —40 dB {—100/+100) MHz <—65 dB <—65 dB C POWER HANDLING: 1 Watt CW, Optional: 10 Watts 1 Microsec Pulse (—AL—) i € | MECHANICAL: t |l > size: DIAMETER: 3.50 in.{£ 88.90 mm] a.se (14733 (.63&1{J|7'1§flpnssiv —ru—) & _1 ‘ . HEIGHT: 0.690 in. [17.53 mm], 0.58" [14.73] (Optlonal for Passive) * 73 (2 C t t : 1 WwEIGHT: §.15 02. (146 Kg) E’ onl FINISH: SKYDROL RESISTANT POLYURETHANE ENAMEL . 0.57" (14.53} (INC), 0.72" [18.29) (N, N—Bulkhead) } BASE IRIDITE PER MIL—C—5441 <4— * "A haebay t n aerhe a , N~—BuiknedG® _, MATERIAL: 6061—76 ALUMINUM ALLOY BASE ©.46°[11.58) (SMA}, 0.837(21.00] (TNC—Bufheod) COMPOSITE RADOME, IMPACT, ABRASION, UV, SOLVENT, € SKYDROL RESISTANCE, AND FIRE RETARDANT | CONNECTOR: SMA FEMALE NAMEPLATE APROXIMATE Location | . figgl%g)r:l%r'rch;cblsfi)ulkhead. N. N Buikhead, C eaaal @ ENVIRONMENTAL: * ‘ —zl. y TEMPERATURE: +87 °F TO 4185 °F 55 °C TO +85 °CJ — 5 448 [3.77] ALTITUCE: 70,000 R. l VIBRATION: > 20 G‘s /— LEAKAGE: HERMETICALLY SEAL 4x 0.190—32 UNC—28 _______ FEDERAL & MILITARY SPECIFICATIONS: 0.250" & ily Spaced on head ggj?fofg‘;:;,a,";a:mmg DESIGN To: FAA TSO—C144, DO—1600, DD—228, MIL—C—5541, M MIL—E—5400, MIL—l—45208A, MIL—STD—810, AND SAE 1455 SMA CONNECTOR ACCEPTANCE TEST PROCEDURE: ATP—GPS—L1L2—100 . |_. (OPTION: TNGC, TNC Bulkhead, 4 |— |vovarnng schews 10—32, 3/4" MSsasasc2re — _ 5 N. N Bulkhead, MCX, MMCX, or Cable} jo—32. 37 255 [6.48] .«.———to s : j . |a/R| — wisuer, custou csms scrsPr00t—6 — 3 Freo pane hk — «ce . . 26Line ... [A WiTk tna ols l s 2. moHD. |15Lt OnLy AL—WiHTHWMAMOIMITER «—— 10| 1 {apnesive caseet 123455—34—530 — 1 3.5" 0A __| PC WitHout ns and thnner mecHreean C _ CT0(—1(—4 pestfirton ~FaRt o ras _ |) (achnit nc 5o=: e 100 0 0_ en wictss ompome Pants ust PIN éG 12_1__1 5>1( xX sies ANTCOM CORP. us |4 « U e OUTLINE_ DRAWING * — — a ist SAAA £ To feu@n 9n ht e 2. MOUNTING SCRews & ADHESIVE CaSKET ARE SUPPUED BY ANTCoM . . tof l m!:‘.:l morvits rr> ds L1 /L2 ACTIVE, OR PASSIVE 1. DIMENSIONS IN BRACKETS ARE IN MLUMETERS [mm] ;:;Ah%sclia woTt ;‘mimNs .w;fg& Wwiilte r7ezs PeR FED.STo sese "&?‘m :{“.:5.:-“ T cl.s GP S ANT_EN N A , xt haQ i mo mac s 3: LUSTERLESS amhy aclzo eERsyaes O * en tm en s wink A| zTA ToR ~ NOTES: uMess omermse spEciFCD; T_—CABLETENGTH (INJ_ . Ms. M NiBuined 3 oLIvE pRas ensen sssom ren reb—sto.soss |_jmome se —d="=»*_—1D| 3CVYE1| 3G1215X—XX—X— . . |R RiGnt ANGLE SGN The—Bukhesd |—¢. LUSTERLESS BLAGK #37030 PER FED—STD—50>8 so wor soaur onimne__| sar 1/ ser j on i _| 7 6 5 4 3 | 2 pe=~e=| 1 PP 17 AnrTAMPFY

anTéon 4)/ 1809001/4 89000 ACTIVE/PASSIVE L1/L2 GPS ANTENNAS PART No. 161215X1000* 261215X1000* 3G1215X1000* 4G1215X1000* Ssize W = 2.07" §Q (5.3 am), D = 2.60" (6.6em), D = 3.50" (8.9cm), W = 2.20" (5.6cm), L = 3.40" (8.6cm), H = 0.64" (1.6cm) H =0.64" (1.6¢m) _H=0.64" (1.6cm) H =0.72" (1.8¢cm) WEIGHT < 5.0 oz (0.142 Kg) *X=A FOR ACTIVE, X=P FOR PASSIVE SPECIFICATIONS ELECTRICAL: FREQUENCY: L1: (1575.42410) MHz L2: (1227.00410) MHz VSWR: 1.5:1 OUTPUT IMPEDANCE: son POLARIZATION: RIGHT HAND CIRCULARLY POLARIZED (RHCP) ANTENNA PATTERN: HEMISPHERICAL DC GROUNDING: YES (LIGHTENING PROTECTION) LNA GAIN: (33.0+/—3.0) dB LNA NOISE FIGURE: <24 dB LNA DRAWING CURRENT: < 60 mA LNA VOLTAGE: (+3.5 TO +24) Volts DC, DIRECT FROM RF CONNECTOR REJECTION: 2 2—POLE FILTERS FOR EACH BAND MECHANICAL: FINISH: SKYDROL RESISTANT POLYURETHANE ENAMEL BASE IRIDITE PER MIL—C—5441 CoLoR: GLOSS WHITE #17925 PER FED—STD—595B LUSTERLESS GRAY #36320 PER FED—STD—595B OLIVE DRAB GREEN #34031 PER FED—STD—595B LUSTERLESS BLACK #37038 PER FED—STD—595B MATERIAL: 6061—T6 ALUMINUM ALLOY BASE THERMOSET PLASTIC RADOME, UV, ABRASION AND SKYDROL RESISTANCE CONNECTOR: SMA FEMALE (TNC, OR N TYPE ISs OPTIONAL) ENVIRONMENTAL: TEMPERATURE: —67°F TO +185°F [—55°C TO +85°CJ ALTITUDE: 70,000 ft. VIBRATION: 10 G‘s LEAKAGE: HERMETICALLY SEAL FEDERAL & MILITARY SPECIFICATIONS: DESIGN TO: FAA TSO—C144, DO—160D, DQ—228, MIL—C—5541, MIL—E—5400, MIL—l—45208A, AND MIL—STD—810 FEATURES: * Suitable for manpack, ground, marine, aircraft, and space applications * Compacts aerodynamic design suitable for harsh environments and long—term operations * Spherical compounded radius—molded radome made of high grade polymer * Design prevents ice/snow buildup, protects antenna from UV, rain and lightning strikes * Chemical, jet fuels, and impact resistance « Meets or exceeds all military specifications and requirements for standard or custom antenna designs + Universal single hole mounting, threaded connector, or magnetic mount, or four 10—32 mounting screws ANTCOM CORPORATION. 1860 Carson Street, Suite 104. Torrance, CA 90501, Tel: 310—782—1076. Fax: 310—782—1086. http:/www.antcom.com LE i— Potorgd ASIENARF


Document Created: 2018-12-17 06:46:45
Document Modified: 2018-12-17 06:46:45
© 2026 FCC.report
This site is not affiliated with or endorsed by the FCC