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VECTOR-600 MIL-STD Tests Details

Test Description Details Test House Date
MIL-STD 810F
MIL-STD 810F, Method 514.5, Procedure I for Category 13 Functional (operation) vibration

Parameter Frequency Functional Specification Requirements (g2/Hz)
f0 90-111.5 0.3
f1 180-223 0.3
f2 360-446 0.075
f3 540-669 0.0336
f4 720-892 0.01875

Test duration: one hour per axis

 INTA Feb 2017
MIL-STD-810F, Method 514.5, Procedure I for Category 13 Endurance vibration

Same curve above with the following levels:

Parameter Frequency Functional Specification Requirements (g2/Hz)
f0 90-111.5 0.405
f1 180-223 0.405
f2 360-446 0.101
f3 540-669 0.0454
f4 720-892 0.02531

Test duration: one hour per axis

 INTA Feb 2017
MIL-STD-810F, Method 514.5, Procedure I for Category 1 Ground transportation vibration test 1
Longitudinal axis: X
Transversal axis: Y
Vertical axis: Z
 
U.S. highway truck vibration exposures figure 514.5C-1
vertical traverse longitudinal
Hz g2/Hz Hz g2/Hz Hz g2/Hz
10 0.01500 10 0.00013 10 0.00650
40 0.01500 20 0.00065 20 0.00650
500 0.00015 30 0.00065 120 0.00020
1.04 g rms 78 0.00002 121 0.00300
  79 0.00019 200 0.00300
  120 0.00019 240 0.00150
  500 0.00001 340 0.00003
  0.204 g rms 500 0.00015
  0.740 g rms

Test duration: one hour per axis

 INTA Feb 2017
MIL-STD-810F, Method 514.5, Procedure I for Category 1 Ground transportation vibration test 2
Longitudinal axis: X
Transversal axis: Y
Vertical axis: Z
 
U.S. highway truck vibration exposures figure 514.5C-1
vertical traverse longitudinal
Hz g2/Hz Hz g2/Hz Hz g2/Hz
5 0.2308 5 0.1373 5 0.0605
8 0.7041 9 0.0900 6 0.0577
12 0.0527 12 0.0902 8 0.0455
16 0.0300 14 0.0427 12 0.0351
20 0.0235 16 0.0496 15 0.0241
22 0.0109 18 0.0229 16 0.0350
24 0.0109 119 0.0008 19 0.0092
26 0.0154 146 0.0013 25 0.0159
69 0.0018 166 0.0009 37 0.0041
79 0.0048 201 0.0009 41 0.0060
87 0.0028 273 0.0053 49 0.0017
123 0.0063 289 0.0021 105 0.0006
161 0.0043 371 0.0104 125 0.0004
209 0.0057 382 0.0019 143 0.0013
224 0.0150 402 0.0077 187 0.0013
247 0.0031 422 0.0027 219 0.0028
278 0.0139 500 0.0016 221 0.0068
293 0.0037 1.60 g rms 247 0.0325
357 0.0028   249 0.0098
375 0.0052   270 0.0026
500 0.0011   293 0.0094
2.18 g rms   336 0.0120
  353 0.0247
  379 0.0085
  431 0.0224
  433 0.0092
  500 0.0014
  1.96 g rms
Test duration: one hour per axis
 INTA Feb 2017
MIL-STD-810F, Method 514.5, Procedure I for Category 10 Sea transportation vibration

All axes

Spectral acceleration distribution
Frequency (Hz) Amplitude (g2/Hz)
5-100 0.0010
Overall acceleration: 0.30 grms

Test duration: two hours per axis

 INTA Feb 2017
MIL-STD-810F, Method 514.5, Procedure I for Category 13 Air transportation vibration

For varying propeller speed, with f0=102Hz (a C130H / J plane), and materiel location “In engine compartment, empennage or pylons”, which define a vibration level L0= 0.60g2/Hz.
 
Parameter Frequency Functional Specification Requirements (g2/Hz)
f0 96.9-117.1 0.6
f1 193.8-214.2 0.1507
f2 290.7-321.3 0.0672
f3 387.6-428.4 0.0379
 
Test duration: one hour per axis
 INTA Feb 2017
MIL-STD-810F, Method 516.5, Procedure I Mechanical shock
Profile for the six semi-axis
Type of shock Saw tooth
Amplitude 15 g
Duration 11 ms
Number of shocks 3 per semi-axis
INTA Feb 2017
The unit shall be submitted to constant acceleration along each direction of the three mutually perpendicular axes, parallel to its principal axes.
 Constant acceleration
Orientation Acceleration (g)
Direction (+X) 15
Direction (-X) 15
Direction (+Y) 10
Direction (-Y) 10
Direction (+Z) 10
Direction (-Z) 10

Minimum duration: 1 minute per axis

 INTA Feb 2017
MIL-STD-810F, Method 501.4, Procedure I
 High Temperature (Storage)
1. Place the test item into the chamber, which will be at ambient conditions.
2. The temperature inside the chamber shall be increased gradually until reaching a temperature of +71 ºC.
3. Maintain the above condition until the stabilization temperature of the test item is reached.
4. Maintain these conditions for 4 hours.
5. The temperature inside the chamber shall be decreased gradually until the ambient conditions are reached.
6. Maintain the above condition until the stabilization temperature of the test item is reached. Then, UAV NAVIGATION personnel will carry out functional tests on the test item.
 INTA Feb 2017
MIL-STD-810F, Method 501.4, Procedure I
 High Temperature (Operation)
1. Place the test item into the chamber, which will be at ambient conditions.
2. The temperature inside the chamber shall be increased gradually until reaching a temperature of +60 ºC.
3. Maintain the above condition until the stabilization temperature of the test item is reached.
4. Maintain these conditions for 2 hours.
5. UAV NAVIGATION personnel switch on the test item.
6. Maintain the above condition until the stabilization temperature of the test item is reached. UAV NAVIGATION personnel will carry out functional tests on the test item. Then, they will switch off the test item.
7. The temperature inside the chamber shall be decreased gradually until the ambient conditions are reached.
8. Maintain the above condition until the stabilization temperature of the test item is reached. Then, UAV NAVIGATION personnel will carry out functional tests on the test item.
 INTA Feb 2017
MIL-STD-810F, Method 502.4, Procedure I
 Low Temperature (Storage)
1. Place the test item into the chamber, which will be at ambient conditions.
2. The temperature inside the chamber shall be decreased gradually until reaching a temperature of -54 ºC.
3. Maintain the above condition until the stabilization temperature of the test item is reached.
4. Maintain these conditions for 4 hours.
5. The temperature inside the chamber shall be increased gradually until the ambient conditions are reached.
6. Maintain the above condition until the stabilization temperature of the test item is reached. Then, UAV NAVIGATION personnel will carry out functional tests on the equipment under test.
 INTA Feb 2017
MIL-STD-810F, Method 501.4, Procedure I
 Low Temperature (Operation)
1. Place the test item into the chamber, which will be at ambient conditions.
2. The temperature inside the chamber shall be decreased gradually until reaching a temperature of -34 ºC.
3. Maintain the above condition until the stabilization temperature of the test item is reached.
4. Maintain these conditions for 2 hours.
5. UAV NAVIGATION personnel switch on the test item, will carry out functional tests on the
equipment under test and then, they will switch off the test item.
6. The temperature inside the chamber shall be increased gradually until the ambient conditions are reached.
7. Maintain the above condition until the stabilization temperature of the test item is reached. Then, UAV NAVIGATION personnel will carry out functional tests on the test item.
 INTA Feb 2017
MIL-STD-810F, Method 500.4, Procedure I
 Altitude (Storage)
1. Place the test item into the chamber, which will be at ambient conditions.
2. The pressure inside the chamber shall be reduced until reaching a pressure of 187 mb (40.000 ft).
3. Maintain these conditions for 1 hour.
4. The pressure inside the chamber shall be increased gradually until ambient conditions are reached.
5. UAV NAVIGATION personnel will carry out functional tests on the equipment under test.
 INTA Feb 2017
MIL-STD-810F, Method 500.4, Procedure II
 Altitude (Operation)
1. Place the test item into the chamber, which will be at ambient conditions.
2. The pressure inside the chamber shall be reduced until reaching a pressure of 465 mb (20.000 ft).
3. Maintain the above condition until the stabilization temperature of the test item is reached.
4. Maintain these conditions for 1 hour. During this time UAV NAVIGATION personnel will carry out functional tests on the equipment under test.
5. The pressure inside the chamber shall be increased gradually until ambient conditions are reached.
6. Maintain the above condition until the stabilization temperature of the test item is reached.
7. UAV NAVIGATION personnel will carry out functional tests on the equipment under test.
 INTA Feb 2017
MIL-STD-810F, Method 500.4, Procedure I
 Humidity
1. Place the test item into the chamber, which will be at ambient conditions.
2. Maintain the chamber temperature at 23 ºC, with the relative humidity at least 50 % for 24 hours.
3. Increase the chamber temperature to +30 ºC and the relative humidity to 95 %.
4. Increase the chamber temperature from +30 ºC to +60 ºC in 4 hours, keeping the relative humidity at 95 %.
5. Maintain these conditions for 6 hour.
6. Decrease the chamber temperature from +60 ºC to +30 ºC in 4 hours, keeping the relative humidity at 95 %.
7. Maintain these conditions for 8 hour.
8. Maintain these conditions for another 4 hours and during this time UAV NAVIGATION personnel will carry out functional tests on the test item.
9. Maintain these conditions for 8 hour.
10. Decrease the chamber temperature to +20 ºC during a period of 1 hour, keeping the relative humidity at 95 %.
11. Maintain these conditions for 4 hours.
12. Increase the chamber temperature to +30 ºC during a period of 1 hour, keeping the relative humidity at 95 %.
13. Maintain these conditions for another 6 hours and during this time UAV NAVIGATION personnel will carry out functional tests on the equipment under test.
14. Repeat the steps 4 to 13 until a total of five cycles (240 hours of exposure) have been completed.
15. Then, UAV NAVIGATION personnel will carry out functional tests on the equipment under test.
 INTA Feb 2017
MIL-STD-461F
MIL-STD-461F, CE102 Conducted Emission Test

SCAN TABLE: "CE102 MIL F ESI40"

Start Frequency Stope Frequency Step Width Detector Meas. Time IF Bandw. Transducer
10.0 kHz 150.0 kHz 500.0 Hz Max Peak 15.0 ms 1 kHz LISN MIL-461F
150.0 kHz 10.0 MHz 5.0 kHz Max Peak 15.0 ms 10 kHz LISN MIL-461F

Operating Conditions: EUT ON POSITIVE NORMAL MODE, EUT OFF VERIFICATION LISN 1239 OUTPUT 1 and EUT ON NEGATIVE NORMAL MODE

 

 INTA 18 Nov 2016
MIL-STD-461F, CS101

Audio-frequency conducted susceptibility

TEST LEVEL: CS101-1. Voltage limit. Curve 2

  • FREQ. RANGE: 30Hz-150KHz
  • FREQ. STEP: 5%
  • DWELL TIME: 3 s
 INTA 23 Nov 2016
MIL-STD-461F, CS114 RF Conducted Susceptibity TEST LEVEL: CURVE 5. MODULATION: PM 1KHz 50%.
  • FREQ. RANGE: 10KHz-200MHz
  • FREQ. STEP: 10kHz - 1MHz 5%, 1MHz – 30MHz 1% and 30MHz – 200MHz 0.5%
  • DWELL TIME: 3 s
 INTA 21 Nov 2016
MIL-STD-461F, CS115 Conducted Susceptibility to impulse excitation TEST LEVEL: 5A INTA 23 Nov 2016
MIL-STD-461F, CS116 Conducted Susceptibility to damped sinusoidal trans. TEST LEVEL: 10A INTA 22 Nov 2016
MIL-STD-461F, RE102 E-field Radiated Emissions
Operating conditions: 
 
Subrange Step Size Detector IF BW Meas Time Transducer
2 MHz-30MHz 5kHz PK+ 10kHz 0.015 s 178
30MHz-200MHz 50kHz PK+ 100kHz 0.015 s 345
200MHz-1GHz 500kHz PK+ 100kHz 0.015 s 1112
1GHz-18GHz 500kHz PK+ 1MHz 0.015 s 697+1221
  • Evaluation of the measurement system (section 5.17.3.4 c. MILSTD-461F). ROD Antenna 178. Freq. = 2MHz
  • Evaluation of the measurement system (section 5.17.3.4 c. MILSTD-461F). ROD Antenna 178. Freq. = 16MHz
  • Evaluation of the measurement system (section 5.17.3.4 c. MILSTD-461F). ROD antenna 178. Freq. = 30MHz
  • Evaluation of the measurement system (section 5.17.3.4 c. MILSTD-461F). Biconnical Antenna 345. Freq. = 200MHz
  • Evaluation of the measurement system (section 5.17.3.4 c. MILSTD-461F). Horn antenna 1112. Freq. = 1GHz
  • Evaluation of the measurement system (section 5.17.3.4 c. MILSTD-461F). Horn antenna 697. + Preamplifier 1221 Freq. = 18GHz
  • EUT OFF. Verification of ambient electromagnetic level (section 4.3.4 MIL-STD-461F). Vertical Polarization
  • EUT OFF. Verification of ambient electromagnetic level (section 4.3.4 MIL-STD-461F). Horizontal Polarization
  • EUT ON. Vertical Polarization
  • EUT ON. Horizontal Polarization
 
 
 INTA 12 Dic 2016
MIL-STD-461F, RS103 E-field Radiated Susceptibility

TEST LEVEL: 100V/m. MODULATION: PM, 1kHz 50%

  • FREQ. RANGE: 2MHz -18GHz
  • FREQ. STEP:
    • 1MHz – 30MHz: 1%
    • 30MHz – 1GHz: 0.5%
    • 1GHz – 18GHz: 0.25%
  • DWELL TIME:. 3 Seg
 
 INTA 14 Dic 2016