Ethernet 2.0 EMC and Environmental Specification Requirement.pdf

Parameter Detail Requirement Test Method

Low Pressure (Altitude)

Storage Sea level to 50,000 ft @ - 57°C

MIL-STD-810G Method 500.5 Procedure I

Operational Sea level to 40,000 ft @ - 54°C

MIL-STD-810G Method 500.5 Procedure II

Explosive Decompression 8,000 ft to 23,100 feet in 8ms

MIL-STD-810G Method 500.5 Procedure IV

High Temperature extremes

Storage, cyclic +95°C MIL-STD-810G Method 501.5 Procedure I

Operational, cyclic +55°C MIL-STD-810G Method 501.5 Procedure II

Operational, constant +71°C for 30 Minutes MIL-STD-810G Method 501.5 Procedure II

Low Temperature extremes

Storage, cyclic -57°C MIL-STD-810G Method 502.5 Procedure I

Operational, cyclic -40°C MIL-STD-810G Method 502.5 Procedure II

Operational, sea level, constant

-65°C for 120 Minutes MIL-STD-810G Method 502.5 Procedure II, as per F-16

Temperature Shock, from constant -54°C to +71°C at 125°C/Minute

MIL-STD-810G Method 503.5 Procedure I-B

Combined temperature-altitude-humidity

Operational, 10 cycles -40°C to +71°C, Sea level to 60,000 ft

MIL-STD-810G Method 520.3 Procedure III

Humidity Operational and Non-Operational, aggravated cycle

95% ± 4% Humidity, +30°C to +60°C, 10 cycles

MIL-STD-810F Method 507.5 Procedure II

Sand and Dust Operational and Non-Operational, blowing

< 150um dust, 150um to 850um sand

MIL-STD-810G Method 510.5 Procedure I (Dust) Procedure II (Sand)

Rain Operational, Dripping 7 gal/ft2/hr, 40 mph for 30 minutes

MIL-STD-810G Method 506.5 Procedure III

Fungus Non-Operational 7-day growth MIL-STD-810G Method 508.6

Salt Fog Operational and Non-Operational, exposure

Four 24-hour wet/dry cycles

MIL-STD-810G Method 509.5

Explosive Atmosphere

Operational At site and 40,000 ft altitudes

MIL-STD-810G Method 511.5 Procedure I

Acceleration, structural

Limit Loads Performance at ±10.0g applied individually along all 3 axes

MIL-STD-810G Method 513.6 Procedure I

Ultimate Loads

Withstand without structural failure ±15.0g applied individually along all 3 axes

MIL-STD-810F Method 513.6 Procedure II

Crash Landing Remain captive, 40g fore, 20g aft and down, 10g up, 18g left and right

MIL-STD-810F Method 513.6 Procedure III

Shock – Functional

Operational

20g, 11ms nominal, 3 blows each direction, each axis (18 total), terminal peak sawtooth

MIL-STD-810G Method 516.6 Procedure I

Shock – Crash Hazard

Non-Operational 40g, 11ms nominal, 2 blows each direction, each axis (12 total)

MIL-STD-810G Method 516.6, Procedure V

Shock – Bench Handling

Non-Operational 4” drop, 1 drop per edge per face (24 total)

MIL-STD-810G Method 516.6, Procedure VI

Vibration

Operational, Performance, Jet aircraft

30 mins, 0.02 g2/Hz to

0.04 g2/Hz, 15 - 2000 Hz, Overall 4.4Grms

MIL-STD-810G Method 514.6, Procedure I, Category 12, Annex D, Fig 514.6D-I

Non-Operational, Endurance, Jet aircraft

60 mins, 0.04 g2/Hz to

0.06 g2/Hz, 15 - 2000 Hz, Overall 9.2Grms

MIL-STD-810G Method 514.6, Procedure I, Category 12, Annex D, Fig 514.6D-I

Operational, Gunfire Shock

7.5 min sweeps, 5 to 15 g, 66 to 856 Hz

MIL-STD-810G Method 519.6, Procedure III

Operational, UH-60 Main Rotor speeds and blade numbers

4 hours, 0.001g2/Hz to 0.01g2/Hz, 3 to 500 Hz

MIL-STD-810G Method 514.6, Procedure I, Category 14, Annex A & Annex D, Table 514.6D-III

Acoustic Noise Operational 30 mins, 140 dB overall, 50 to 10000 Hz

MIL-STD-810G Method 515.6 Procedure I

Conducted Emissions

Operational Power Leads, 30 Hz to 10 kHz

MIL-STD-461G CE101

Par 5.4, CE101-4 Curve #2

Operational Power Leads, 10 kHz to 10MHz

MIL-STD-461G CE102

Par 5.5, Fig CE102-1 Basic Curve

Conducted Susceptibility

Operational Power leads, 30Hz to 150 kHz

MIL-STD-461G CS101

Par 5.7, Fig CS101-1 Curve #2

Operational Bulk cable injection, 10 kHz to 200MHz

MIL-STD-461G CS114

Par 5.12, Fig CS114-1 Curve #5

Operational Bulk cable injection, impulse excitation, 30Hz for one minute

MIL-STD-461G CS115

Par 5.13, Fig CS115-1

Operational

Damped sinusoidal transients, cables and power leads, 10kHz to 100MHz, 5 minutes

MIL-STD-461G CS116

Par 5.14, Fig CS116-1 and CS116-2

Radiated Emissions

Operational Magnetic field, 30Hz to 100kHz

MIL-STD-461G RE101

Par 5.17, Fig RE101-1 and Fig

RE101-2

Operational Electric field, 10kHz to 18GHz

MIL-STD-461G RE102

Par 5.18, Fig RE102-3 Fixed wing external and Fixed wing internal < 25m

Radiated Susceptibility

Operational Magnetic field, 30 Hz to 100 kHz

MIL-STD-461G RS101

Par 5.20 Fig RS101-2 Army

Operational Electric field, 2 MHz to 18 GHz

MIL-STD-461G RS103

Par 5.21, Table XI, Aircraft Internal Army

Power Supply

Operational, normal condition

Load measurements, ask for info

MIL-STD-704F Chg1

MIL-HDBK-704-8 LDC-101

Operational, normal condition

Steady state limits, 22 Vdc to 29 Vdc

MIL-STD-704F Chg1

MIL-HDBK-704-8 LDC-102

Tests A, B, C

Operational, normal condition

Voltage distortion spectrum

MIL-STD-704F Chg1 Fig 15

MIL-HDBK-704-8 LDC-103

Tests A thru K

Operational, normal condition

Total ripple MIL-STD-704F Chg1 Fig 15

MIL-HDBK-704-8 LDC-104,

Table LDC104-II

Operational, normal condition

Normal voltage transients, 18Vdc to 29Vdc

MIL-STD-704F Chg1 Fig 13

MIL-HDBK-704-8 LDC-105

Tests AA thru RR

Operational, transfer interrupt

Power interrupt, 50ms, 22Vdc to 29Vdc

MIL-HDBK-704-8 LDC-201

Operational, abnormal condition

Steady state limits, 20.0 Vdc and 31.5Vdc, 30 minutes

MIL-STD-704F Chg1

MIL-HDBK-704-8 LDC-301

Tests A and B

Operational, abnormal condition

Abnormal voltage transients, abnormal condition

MIL-STD-704F Chg1 Fig 14

MIL-HDBK-704-8 LDC-302,

Tests AAA thru NNN, 7 to 50V

Operational, emergency condition

Steady state limits, 18 Vdc to 29 Vdc

MIL-HDBK-704-8 LDC-401

Operational, starting Starting voltage transients, 12 Vdc to 29 Vdc

MIL-STD-704F Chg1

MIL-HDBK-704-8 LDC-501,

Table LDC501-IV

Operational, power failure and automatic recovery

Power failure, from 100ms to 7 seconds

MIL-STD-704F Chg1

MIL-HDBK-704-8 LDC-601

Tests A thru D

Operational, power failure

Phase reversal protection/prevention

MIL-STD-704F Chg1

MIL-HDBK-704-8 LDC-602

Max Power Use

Operational, startup, all ports negotiating link

≤ 56W

Operational, steady-state, all ports on at max speed

≤ 29W

Operational, steady-state, 3 10GbE on at max speed, 4 1GbE ports on at max speed, all other ports on at 100Mbps

≤ 21W

Operational, steady-state, only 16 1GbE ports on at max speed

≤ 19W

Chassis Grounding

Operating

Allow for proper electrical bonding through designated external stub and dedicated pins on connectors

SAE-AS-50881H

Electrical Bonding

Operating

Primary Chassis ground connection for electrical bonding provided by designated external stub

MIL-STD-464C, Paragraph 5.11.3

Mounting For vibration tolerance 4x 10-32 captive screws