GES – Users Manual
Page 30 of 33
11. Qualifications
Characteristic
Ports
Dimensions
Weight
Management
Connectors
Military Specification
Test Detail Comment/Tailoring
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
MIL-STD-810F Method 507.4
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
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
MIL-STD-810F Method 516.5, Procedure VI
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
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
Power leads, 10 kHz to 10MHz
Power leads, 30Hz to 150 kHz
Bulk cable injection, 10 kHz to 200MHz
Bulk cable injection, impulse excitation
Damped sinusoidal transients, cables and power leads, 10kHz to 100MHz
Electric field, 30Hz to 100KHz
Electric field, 2MHz to 18GHz
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 < 2.5mΩ
DC resistance measured between each power input line and the safety grounding contact > 1MΩ
12 - 1000Mbps full duplex,10Mbps or 100Mbps full or half duplex
Management Processor available for custom configurations
MIL-C-38999 (Signal and Power)
MIL-STD-810F Method 501.4 Procedure II
MIL-STD-810F Method 513.5 Procedure I
Acceleration Load Factors
Electromagnetic Compatibility
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General