GES – Users Manual
Page 30 of 33
11. Qualifications
Characteristic
Ports
Dimensions
Weight
Management
Connectors
Military Specification
Test
Detail
Comment/Tailoring
MIL-HDBK-5400
Cooling Air
Free Air, unmounted
Does not use the aircraft structure as a heat sink
MIL-STD-810F Method 500.4 Procedure I
Storage
Procedure I: -57°C @ 40,000 feet
MIL-STD-810F Method 500.4 Procedure II
Operational
Procedure II : -40°C @ 40,000 feet
MIL-STD-810F Method 500.4 Procedure IV
Explosive Decompression Procedure IV: 8,000 feet to 23,100 feet in 0.008mSec
MIL-STD-810F Method 501.4 Procedure I
Storage
Procedure I: +95°C
Operational
Procedure II: +55°C
Operational
Procedure II: +71°C for 30 Minutes
MIL-STD-810F Method 502.4 Procedure I
Storage
Procedure I: -57°C
MIL-STD-810F Method 502.4 Procedure II
Operational
Procedure II: -40°C
MIL-STD-810F Method 503.4, Procedure I
Temperature Shock
-40°C - +55°C at 20°C/Minute
MIL-STD-810F Method 506.4 Procedure III
Rain
MIL-STD-810F Method 507.4
Humidity
Operating and non-operating effects of humidity, including conditions wherein condensation takes place in and on
the equipment
MIL-STD-810F Method 508.5
Fungus
Designed with certified fungus inert materials
MIL-STD-810F Method 509.4 Procedure I
Salt Fog
Operating and non-operating exposure to salt-sea atmosphere
MIL-STD-810F Method 510.4 Procedure I & II
Sand and Dust
MIL-STD-810F Method 511.4 Procedure I
Explosive Atmosphere
At site and 40,000ft altitudes
Limit Loads
Performance at
±
10.0G applied individually along the three axes
Ultimate Loads
Withstand without structural failure
±
15.0G applied individually along the three axes
Crash Landing
Remain captive, 40G forward, 20G aft and down, 14G left/right, 10G up
MIL-STD-810F Method 514.5 Performance
Vibration
Performance
0.025 G2/Hz 300 - 1000 Hz, Overall 4.4Grms
MIL-STD-810F Method 514.5 Endurance
Vibration
Endurance
0.06 G2/Hz 300 - 1000 Hz, Overall 9.2Grms
MIL-STD-810F Method 514.5 Gunfire
Vibration
Gunfire Sine Sweeps
Up to 15G
MIL-STD-810B Method 515.1 Category B
Acoustical Noise
140db
MIL-STD-810F Method 516.5, Procedure VI
Bench Handling
MIL-STD-810F Method 516.5 Procedure I
Functional
As modified: eighteen (18) blows, terminal peak sawtooth, 20g, 11ms
MIL-STD-810F Method 516.5, Procedure V
Crash Safety
TPS (terminal peak sawtooth), 40g, 11 millisecond shock as modified by MIL-STD-810B, Method 516, Procedure
III Figure 516-1
MIL-STD-810F Method 520.2 Procedure III
Temperature Altitude
Operational at 60,000 feet from -40°C to +23°C, 33,000 feet at +55°C
MIL-HDBK-217 FN2, Method I, Case 3 using part stress
calculations. 100% Duty Cycle
MTBF
8,474 hours @ +55°C, Airborne Uninhabited Fighter Environment
Transportability
Transportation by rail, truck, air and/or ship at altitudes up to 45,000 ft.
Service Life
>10,000 hours
Mounting
Self locking, Retained
MIL-STD-704A 28VDC Category B
Curve 2 and Curve 3 of Figure 9 < 22Watts
CE101
Power leads, 30Hz to 10KHz
CE102
Power leads, 10 kHz to 10MHz
CS101
Power leads, 30Hz to 150 kHz
CS114
Bulk cable injection, 10 kHz to 200MHz
CS115
Bulk cable injection, impulse excitation
CS116
Damped sinusoidal transients, cables and power leads, 10kHz to 100MHz
RE101
Electric field, 30Hz to 100KHz
RE102
Electric field, 2MHz to 18GHz
MIL-STD-461F
RS103
Radiated Susceptibility 20 V/m from 30MHz to 1GHz - 60V/m from 1GHz to 18GHz
SAE ARP 1870
Electrical Bonding
DC resistance measured from the equipment case to the aircraft structure < 2.5m
Ω
DC resistance measured between each power input line and the safety grounding contact > 1MΩ
Detail
12 - 1000Mbps full duplex,10Mbps or 100Mbps full or half duplex
8.25" x 5.1" x 1.38"
Management Processor available for custom configurations
Radiated Emissions
MIL-C-38999 (Signal and Power)
2 lb 12 oz (1.25 kg)
Environmental
Altitude
MIL-STD-461F
Conducted Susceptibility
Chassis Grounding
MIL-STD-810F Method 501.4 Procedure II
MIL-STD-461F
Primary Power
Low Temperature
High Temperature
MIL-STD-810F Method 513.5 Procedure I
Acceleration Load Factors
Electromagnetic Compatibility
Shock
MIL-STD-461F
Conducted Emissions
