MIL-STD 461F Results for M&A Technology Companion epad Computer
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1 11 July 11 MIL-STD 461F Results for M&A Technology Companion epad Computer Prepared For: Mike Lehner M&A Technology Chenault Dr Carrolton, TX 6 Prepared By: John C. Zentner Test Engineer Integrated Demonstrations & Applications Laboratory (IDAL) Electromagnetic Interference (EMI) Research Laboratory AFRL/RYWD WPAFB, OH Approved By: Manuel Rodriguez, Technical Advisor Electromagnetic Environmental Effects Defense Systems & Electronic Sensors Branch Engineering Directorate
2 Table of Contents 1.0 EXECUTIVE SUMMARY References Requirements Summary of Results GENERAL Item Description Modes of Operation Facility Test Setups MEASUREMENT RESULTS CE2 - Conducted Emissions, Power Leads, khz to MHz CE2 Measurement Conditions CE2 Results CE2 EUT Measurement Scans CE2 System Accuracy Scans RE2 - Radiated Emissions, Electric Field, 2 MHz to 18GHz RE2 Measurement Conditions RE2 Results RE2 EUT Measurement Scans RE2 System Accuracy Scans RE2 Ambient Scans... 43
3 Level (dbµv) 1.0 Executive Summary 1.1 References MIL-STD-461F, Requirements for the Control of Electromagnetic Interference Characteristics of Equipment and Subsystems, December Requirements The M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter were evaluated with respect to the following MIL-STD-461F requirements. CE2 - Conducted Emissions, Power Leads, khz to MHz RE2 - Radiated Emissions, Electric Fields, 2 MHz to 18 GHz 1.3 Summary of Results. The equipment complies with the CE2 limit with the minor exception shown below. 0 CE2 1VAC 90 k k k 90 k 0 k 1 k 1 k 1 k 1 k 1 k Significant RE2 emissions that alone influence where the equipment can be operated are as follows. The Companion epad with AC/DC adapter exceeds the RE2 limit for helicopters from 2 to 36 MHz. Portions of the frequency range are over the RE2 limit for small-body fixed-wing aircraft (< meters nose-to-tail). Under battery operation, almost all emissions are below the helicopter limit in all frequency ranges The equipment adequately meets emission requirements for certification for use on Air Force fixed-wing aircraft when connected to aircraft 1 Volt AC power and for all Air Force aircraft under internal battery operation.
4 2.0 General 2.1 Item Description The equipment under test was an M&A Technology Companion epad computer and Delta ADP- PH AC/DC Adapter. The equipment will be used during flight. The equipment is shown below. Companion epad Computer Front Companion epad Computer Back
5 ADP-PH AC/DC Adapter 2.2 Modes of Operation The Companion epad was turned on with the Windows Desktop displayed. Complete data scans were taken with the computer powered by the AC/DC adapter (1 Volts, Hz). Additional measurements were accomplished under battery operation where possibly improved results were anticipated. 2.3 Facility The measurements were performed in a foot x 18 foot x foot shielding room. The room is treated with anechoic material in accordance with MIL-STD-461F requirements. For CE2 and RE2, test instrumentation was located in a separate shielded control room. 2.4 Test Setups The general test setup was as shown below.
6 LISNs General Setup A standard test equipment item used during all testing was a Line Impedance Stabilization Networks (LISNs) inserted in the power leads per MIL-STD-461F. The network has two sections, one for the high side of the power and a second for the return side. Common Test Equipment Manufacturer Model Function Serial # Calibration Due Date Fischer Custom FCC-LISN-3 LISN 323 NCR Communications Hewlett Packard 3314A Function Generator A /02/11 Calibration requirements and designations per the US Air Force Calibration Authority
7 3.0 Measurement Results 3.1 CE2 - Conducted Emissions, Power Leads, khz to MHz CE2 Measurement Conditions The Companion epad and ADP-PH AC/DC Adapter and measurement conditions were set up in accordance with MIL-STD-461F requirements. The instrumentation used is listed below. CE2 Test Equipment Manufacturer Model Function Serial Number Cal Due Hewlett Packard 8566B Spectrum Analyzer 19A /29/11 Hewlett Packard 85685A Preselector 36A084 NCR Hewlett Packard 3314A Function Generator, MHz A /2/11 LeCroy 2 Digitizing Oscilloscope 01J /9/12 Aeroflex db Attenuator BX //12 Calibration requirements and designations per the US Air Force Calibration Authority NCR - No Calibration Required Measurements were performed at the Line Impedance Stabilization Network (LISN) on each power lead. The bandwidths and sweep times used are listed below. Bandwidths & Sweep Times Frequency Range (MHz) Resolution BW - 3 db (khz) Video BW 3 db (khz) Sweep Time (Seconds) In accordance with MIL-STD-461F, system accuracy measurements are performed prior to testing to ensure that the measurement system will produce accurate results. Test frequencies and voltage levels that are injected at the power lead connections to the LISNs are shown below. The injected level is 6 db below the MIL-STD-461F limit and is calculated as a peak-to-peak voltage measured on an oscilloscope. Measurement System Test Frequency (MHz) Limit (dbµv) Limit - 6 db (dbµv) Limit - 6 db (mv rms) Limit - 6 db (mv peak-peak) Photos of the setups at the line impedance stabilization networks are shown below.
8 Power Return Signal Injection for Calibration Power High Power Return Testing Power High
9 Level (dbµv) Level (dbµv) CE2 Results CE2 EUT Measurement Scans CE2: - khz. High side of input power. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/9/11 1:12:29 PM 1 CE2 1VAC 0 90 k k k k k k CE2: - 1 khz. High side of input power. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/9/11 1:13: PM 0 CE2 1VAC 90 k k k 90 k 0 k 1 k 1 k 1 k 1 k 1 k
10 Level (dbµv) Level (dbµv) CE2: 1-0 khz. High side of input power. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/9/11 1:14:18 PM 90 CE2 1VAC 1 k 0 k 2 k 0 k 3 k 0 k 4 k 0 k 5 k 0 k CE2: MHz. High side of input power. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/9/11 1::03 PM CE2 1VAC 75 0 k 0 k 00 k 1.2 M 1.4 M 1.6 M 1.8 M 2.0 M
11 Level (dbµv) Level (dbµv) CE2: 2 - MHz. High side of input power. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/9/11 1::46 PM CE2 1VAC 75 2 M 3 M 4 M 5 M 6 M 7 M 8 M 9 M M CE2: - khz. Return side of input power. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/9/11 1:17:19 PM 1 CE2 1VAC 0 90 k k k k k k
12 Level (dbµv) Level (dbµv) CE2: - 1 khz. Return side of input power. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/9/11 1:18:03 PM 0 CE2 1VAC 90 k k k 90 k 0 k 1 k 1 k 1 k 1 k 1 k CE2: 1-0 khz. Return side of input power. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/9/11 1:07:47 PM 90 CE2 1VAC 1 k 0 k 2 k 0 k 3 k 0 k 4 k 0 k 5 k 0 k
13 Level (dbµv) Level (dbµv) CE2: MHz. Return side of input power. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/9/11 1:08: PM CE2 1VAC 75 0 k 0 k 00 k 1.2 M 1.4 M 1.6 M 1.8 M 2.0 M CE2: 2 - MHz. Return side of input power. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/9/11 1:09:19 PM CE2 1VAC 75 2 M 3 M 4 M 5 M 6 M 7 M 8 M 9 M M
14 Level (dbµv) CE2 System Accuracy Scans The following scans are performed to verify the integrity of the measurement setup prior to testing. A calibrated signal is applied at the EUT power connection at each LISN at a level that is 6 db below the MIL-STD-461 limit. The indicated level on the plot should be 6 db +/- 3 db from the limit line. CE2: - khz,.5 khz. High side of input power. Time of Measurement: 7/9/11 12:36:52 PM 1 CE2 1VAC 0 90 k k k k k k
15 Level (dbµv) Level (dbµv) CE2: - 1 khz, 0 khz. High side of input power. Time of Measurement: 7/9/11 12::06 PM 90 CE2 1VAC k k k 90 k 0 k 1 k 1 k 1 k 1 k 1 k CE2: MHz, 1.95 MHz. High side of input power. Time of Measurement: 7/9/11 12:33:59 PM CE2 1VAC 75 0 k 0 k 00 k 1.2 M 1.4 M 1.6 M 1.8 M 2.0 M
16 Level (dbµv) Level (dbµv) CE2: 2 - MHz, 9.8 MHz. High side of input power. Time of Measurement: 7/9/11 12:33:01 PM CE2 1VAC 75 2 M 3 M 4 M 5 M 6 M 7 M 8 M 9 M M CE2: - khz,.5 khz. Return side of input power. Time of Measurement: 7/9/11 12:28:13 PM 1 CE2 1VAC 0 90 k k k k k k
17 Level (dbµv) Level (dbµv) CE2: - 1 khz, 0 khz. Return side of input power. Time of Measurement: 7/9/11 12:29:21 PM 90 CE2 1VAC k k k 90 k 0 k 1 k 1 k 1 k 1 k 1 k CE2: MHz, 1.95 MHz. Return side of input power. Time of Measurement: 7/9/11 12::18 PM CE2 1VAC 75 0 k 0 k 00 k 1.2 M 1.4 M 1.6 M 1.8 M 2.0 M
18 Level (dbµv) CE2: 2 - MHz, 9.8 MHz. Return side of input power. Time of Measurement: 7/9/11 12:: PM CE2 1VAC 75 2 M 3 M 4 M 5 M 6 M 7 M 8 M 9 M M
19 3.2 RE2 - Radiated Emissions, Electric Field, 2 MHz to 18GHz RE2 Measurement Conditions The TUFFnote computer and FPS0-RAB AC/DC Adapter and the measurement conditions were set up in accordance with MIL-STD-461F requirements. The instrumentation used is listed below. RE2 Test Equipment Manufacturer Model Function Serial # Cal Due Date Hewlett Packard 8566B Spectrum Analyzer 19A /29/11 Hewlett Packard 85685A Preselector 36A084 NCR Miteq AFS42- Preamplifier NCR P-42-L ETS Lindgren 31B Rod Antenna NPC EMCO 39 Biconical Antenna ICO EMCO 36 Double Ridge Guide 27 NPC Ant EMCO 31 Double Ridge Guide Ant 2177 NCR Hewlett Packard 8642B Signal Generator 2647A001 3//12 Hewlett Packard 8763E Signal Generator 2821A /12/11 Electro-Metrics EM-6888 Stub Radiator 7901 NCR Calibration requirements and designations per the US Air Force Calibration Authority NCR - No Calibration Required NPC - No Periodic Calibration Required ICO - Initial Calibration Only Required All antennas were positioned 1 meter from the EUT. Measurements above MHz were performed in both vertical and horizontal antenna polarity positions. The bandwidths and sweep times used are listed below. Bandwidths & Sweep Times Frequency Band (MHz) Resolution BW - 3 db (khz) Video BW - 3 db (khz) Sweep Times (Seconds) Number of Sweeps
20 Commercial software is used for testing. The program is Dare Development s RadiMation package, Version The antennas factors for the measurement antennas as stored in the software are shown below. EMCO 31B Monopole EMCO 39 Biconical
21 EMCO 36 Double Ridge Guide EMCO 31 Double Ridge Guide The cable loss from the antenna to the measurement receiver as stored in the software is shown below. The loss was measured using a signal source and power meter. A reference level was first established on the power meter at each frequency. The entire cable was then inserted and the power level again measured. The difference is the cable loss. Cable Loss - Semflex Coax A preamplifier is used between 1 and 18 GHz to improve the sensitivity of the measurement system. The gain as stored in the software is shown below. 21
22 Miteq Gain, 1 to 18 GHz Information used to determine the drive level for system accuracy scans is shown below. The limit that is used is for RE2 small-fixed wing, aircraft applications. Injected levels in dbm are calculated as follows: Frequency (MHz) A B = A - 6 C D = B - C E = D - 7 Limit (dbuv/m) Limit less 6 db (dbuv/m) Antenna Factor (db/m) Injected Level (dbuv) Injected Level (dbm) Remarks Antenna factor for signal injection purposes is 1/2 m height of rod Antenna factor for signal injection purposes is 1/2 m height of rod Antenna factor for signal injection purposes is 1/2 m height of rod Photos of setups with the various antennas are shown below. 22
23 Rod Antenna, 2 to MHz Vertical Polarization Biconical Antenna, to 0 MHz Horizontal Polarization 23
24 Vertical Polarization Double Ridge Guide Antenna, 0 to 00 MHz Horizontal Polarization Vertical Polarization Horizontal Polarization Double Ridge Guide Antenna, 1 to 18 GHz 24
25 Level (dbµv/m) Level (dbµv/m) RE2 Results RE2 EUT Measurement Scans RE2: 2-8 MHz. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/11/11 11:33:26 AM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter 2 M 3 M 4 M 5 M 6 M 7 M 8 M RE2: 8 - MHz. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/11/11 11:34:12 AM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter 8.0 M M M M M M
26 Level (dbµv/m) Level (dbµv/m) RE2: 2-8 MHz. M&A Technology Companion epad computer powered by internal batteries. Time of Measurement: 7/11/11 11:36: AM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter M 3 M 4 M 5 M 6 M 7 M 8 M RE2: 8 - MHz. M&A Technology Companion epad computer powered by internal batteries. Time of Measurement: 7/11/11 11:37:22 AM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter M M M M M M 26
27 Level (dbµv/m) Level (dbµv/m) RE2: - 90 MHz. Antenna polarity: Vertical. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/11/11 6:59:59 AM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter 5 0 M M M M M M 90 M RE2: - 90 MHz. Antenna polarity: Horizontal. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/11/11 7:03:52 AM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter 5 0 M M M M M M 90 M 27
28 Level (dbµv/m) Level (dbµv/m) RE2: - 90 MHz. Antenna polarity: Vertical. M&A Technology Companion epad computer powered by internal batteries. Time of Measurement: 7/11/11 7:08:32 AM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter 5 0 M M M M M M 90 M RE2: - 90 MHz. Antenna polarity: Horizontal. M&A Technology Companion epad computer powered by internal batteries. Time of Measurement: 7/11/11 7:07: AM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter 5 0 M M M M M M 90 M 28
29 Level (dbµv/m) Level (dbµv/m) RE2: 90-1 MHz. Antenna polarity: Vertical. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/11/11 7:00:57 AM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter M 95 M 0 M 5 M 1 M 1 M 1 M RE2: 90-1 MHz. Antenna polarity: Horizontal. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/11/11 7:04:43 AM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter M 95 M 0 M 5 M 1 M 1 M 1 M 29
30 Level (dbµv/m) RE2: 90-1 MHz. Antenna polarity: Vertical. M&A Technology Companion epad computer powered by internal batteries. Time of Measurement: 7/11/11 7:09:18 AM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter M 95 M 0 M 5 M 1 M 1 M 1 M
31 Level (dbµv/m) Level (dbµv/m) RE2: 1-0 MHz. Antenna polarity: Vertical. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/11/11 7:01:36 AM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter 1 M 1 M 1 M 1 M 1 M 1 M 1 M 190 M 0 M RE2: 1-0 MHz. Antenna polarity: Horizontal. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/11/11 7:05:19 AM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter 1 M 1 M 1 M 1 M 1 M 1 M 1 M 190 M 0 M 31
32 Level (dbµv/m) Level (dbµv/m) RE2: 0-0 MHz. Antenna polarity: Vertical. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/9/11 2:47:32 PM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter 0 M 2 M 0 M 3 M 0 M RE2: 0-0 MHz. Antenna polarity: Horizontal. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/9/11 2:51:59 PM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter 0 M 2 M 0 M 3 M 0 M 32
33 Level (dbµv/m) Level (dbµv/m) RE2: 0-00 MHz. Antenna polarity: Vertical. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/9/11 2:48:41 PM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter 0 M 0 M 0 M 0 M 0 M 900 M 00 M RE2: 0-00 MHz Hor. Antenna polarity: Horizontal. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/9/11 2:53:29 PM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter 0 M 0 M 0 M 0 M 0 M 900 M 00 M 33
34 Level (dbµv/m) Level (dbµv/m) RE2: 1-2 GHz. Antenna polarity: Vertical. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/11/11 8:17:58 AM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter M 1.2 G 1.4 G 1.6 G 1.8 G 2.0 G RE2: 1-2 GHz. Antenna polarity: Horizontal. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/11/11 8:14:28 AM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter M 1.2 G 1.4 G 1.6 G 1.8 G 2.0 G 34
35 Level (dbµv/m) Level (dbµv/m) RE2: 2-4 GHz. Antenna polarity: Vertical. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/11/11 :19:42 AM 90 Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter G 2.5 G 3.0 G 3.5 G 4.0 G RE2: 2-4 GHz. Antenna polarity: Horizontal. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/11/11 :13:31 AM 90 Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter G 2.5 G 3.0 G 3.5 G 4.0 G
36 Level (dbµv/m) Level (dbµv/m) RE2: 4-8 GHz. Antenna polarity: Vertical. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/11/11 ::48 AM 90 Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter G 4.5 G 5.0 G 5.5 G 6.0 G 6.5 G 7.0 G 7.5 G 8.0 G RE2: 4-8 GHz. Antenna polarity: Horizontal. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/11/11 :26: AM 90 Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter G 4.5 G 5.0 G 5.5 G 6.0 G 6.5 G 7.0 G 7.5 G 8.0 G 36
37 Level (dbµv/m) Level (dbµv/m) RE2: 8-12 GHz. Antenna polarity: Vertical. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/11/11 :22:22 AM 0 Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter G 8.5 G 9.0 G 9.5 G.0 G.5 G 11.0 G 11.5 G 12.0 G RE2: 8-12 GHz. Antenna polarity: Horizontal. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/11/11 :14:26 AM 0 Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter G 8.5 G 9.0 G 9.5 G.0 G.5 G 11.0 G 11.5 G 12.0 G 37
38 Level (dbµv/m) Level (dbµv/m) RE2: GHz. Antenna polarity: Vertical. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/11/11 :23:58 AM 0 Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter G 13.0 G 14.0 G.0 G 16.0 G 17.0 G 18.0 G RE2: GHz. Antenna polarity: Horizontal. M&A Technology Companion epad computer and Delta ADP-PH AC/DC Adapter powered by 1 Volt, Hz. Time of Measurement: 7/11/11 :16:00 AM 0 Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter G 13.0 G 14.0 G.0 G 16.0 G 17.0 G 18.0 G 38
39 Level (dbµv/m) RE2 System Accuracy Scans The following scans are performed to verify the integrity of the measurement setup prior to testing. A calibrated signal is applied at the antenna connection that is equivalent to a level that is 6 db below the MIL-STD-461 limit. The indicated level on the plot should be 6 db +/- 3 db from the limit line. RE2: 2-8 MHz, 2.1 MHz. System accuracy. The indicated level on the plot should be 6 db +/- 3 db from the limit line. Time of Measurement: 7/11/11 11:11:51 AM Fixed-Wing Aircraft < m Nose-to-Tail M 3 M 4 M 5 M 6 M 7 M 8 M 39
40 Level (dbµv/m) Level (dbµv/m) RE2: 8 - MHz, 12 MHz. System accuracy. The indicated level on the plot should be 6 db +/- 3 db from the limit line. Time of Measurement: 7/11/11 11:12:41 AM Fixed-Wing Aircraft < m Nose-to-Tail M M M M M M RE2: 8 - MHz, 29.5 MHz. System accuracy. The indicated level on the plot should be 6 db +/- 3 db from the limit line. Time of Measurement: 7/11/11 11:13:31 AM Fixed-Wing Aircraft < m Nose-to-Tail M M M M M M
41 Level (dbµv/m) Level (dbµv/m) RE2: 1-0 MHz, 197 MHz. System accuracy. The indicated level on the plot should be 6 db +/- 3 db from the limit line. Time of Measurement: 7/11/11 6:42: AM Fixed-Wing Aircraft < m Nose-to-Tail M 1 M 1 M 1 M 1 M 1 M 1 M 190 M 0 M RE2: 0-00 MHz, 990 MHz. System accuracy. The indicated level on the plot should be 6 db +/- 3 db from the limit line. Time of Measurement: 7/9/11 3::22 PM Fixed-Wing Aircraft < m Nose-to-Tail 0 M 0 M 0 M 0 M 0 M 900 M 00 M 41
42 Level (dbµv/m) Level (dbµv/m) RE2: 1-2 GHz, 1.95 GHz. System accuracy. The indicated level on the plot should be 6 db +/- 3 db from the limit line. Time of Measurement: 7/11/11 7:44:44 AM Fixed-Wing Aircraft < m Nose-to-Tail 00 M 1.2 G 1.4 G 1.6 G 1.8 G 2.0 G RE2: GHz, 17.5 GHz. System accuracy. The indicated level on the plot should be 6 db +/- 3 db from the limit line. Time of Measurement: 7/11/11 8:26:38 AM 90 Fixed-Wing Aircraft < m Nose-to-Tail G 13.0 G 14.0 G.0 G 16.0 G 17.0 G 18.0 G 42
43 Level (dbµv/m) RE2 Ambient Scans The following scans are performed to measure the conditions in the shielded room with the EUT turned off. Measured levels should be at least 6 db below the MIL-STD-461 limit. RE2: 2 - MHz Ambient. Time of Measurement: 7/11/11 11::24 AM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter M 5 M M M M M M 43
44 Level (dbµv/m) Level (dbµv/m) RE2: - 0 MHz Ambient. Antenna polarity: Vertical. Time of Measurement: 7/11/11 6:44: AM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter 5 0 M M M 0 M 1 M 1 M 1 M 1 M 0 M RE2: - 0 MHz Ambient. Antenna polarity: Horizontal. Time of Measurement: 7/11/11 6::54 AM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter 5 0 M M M 0 M 1 M 1 M 1 M 1 M 0 M 44
45 Level (dbµv/m) Level (dbµv/m) RE2: 0-00 MHz Ambient. Antenna polarity: Vertical. Time of Measurement: 7/9/11 3:13: PM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter 0 0 M 0 M 0 M 0 M 0 M 0 M 0 M 900 M 00 M RE2: 0-00 MHz Ambient. Antenna polarity: Horizontal. Time of Measurement: 7/9/11 3:17:14 PM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter 0 0 M 0 M 0 M 0 M 0 M 0 M 0 M 900 M 00 M
46 Level (dbµv/m) Level (dbµv/m) RE2: 1-2 GHz Ambient. Antenna polarity: Vertical. Time of Measurement: 7/11/11 7:46:44 AM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter M 1.2 G 1.4 G 1.6 G 1.8 G 2.0 G RE2: 1-2 GHz Ambient. Antenna polarity: Horizontal. Time of Measurement: 7/11/11 7:47:57 AM Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter M 1.2 G 1.4 G 1.6 G 1.8 G 2.0 G 46
47 Level (dbµv/m) Level (dbµv/m) RE2: 2-18 GHz Amb. Antenna polarity: Vertical. Time of Measurement: 7/11/11 9:16:24 AM 0 Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter 90 2 G 4 G 6 G 8 G G 12 G 14 G 16 G 18 G RE2: 2-18 GHz. Antenna polarity: Horizontal. Time of Measurement: 7/11/11 9:04:49 AM 0 Fixed-Wing Aircraft >= m Nose-to-Tail Fixed-Wing Aircraft < m Nose-to-Tail Helicopter 90 2 G 4 G 6 G 8 G G 12 G 14 G 16 G 18 G 47
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