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Crew
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2 pilots
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Height
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12 feet 10.6 inches
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Length
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41 feet 2.4 inches
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Rotor diameter
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35 feet
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Maximum gross weight
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4,500 pounds (unarmed);
5,500 pounds (armed)
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Maximum airspeed
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125 KIAS
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Cruise airspeed
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80 KIAS
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Endurance
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2 hours
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Cargo hook capacity
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2,000 pounds
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Litter capacity
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4 (externally)
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Troop-carrying capacity
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6 (externally).
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Avionics
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Data transfer system ground station, data transfer module, data transfer receptacle in the aircraft.
Video tape recorder records up to 2 hours of copilot's MFD.
ANVIS display symbology system provides basic flight information.
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Mast-mounted sight
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Thermal imaging sensor.
Television sensor.
Laser range finder/designator.
Optical boresight system.
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Weapons
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.50-caliber heavy machine gun.
70-millimeter folding fin aerial rocket.
Air-to-air Stinger missile.
Hellfire modular missile system.
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Communication equipment
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Two VHF-FM AN/ARC-186 or AN/ARC-201 SINCGARS.
One UHF AN/ARC-164 Have Quick.
One VHF-AM AN/ARC-186.
Two TSEC/KY-58.
HF capable (radio not installed).
TSEC/KY-75 (device not installed).
Retransmission capabilities.
FM homing (AN/ARC-186 only).
Airborne target handover system (digital communications).
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Navigation equipment
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Attitude and heading reference system (Litton LR-80 Inertial).
AN/ASN-137 doppler.
AN/ASN-43 directional gyro.
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Aircraft survivability equipment
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AN/APX-100 IFF.
AN/ALQ-144 IR jammer.
AN/APR-39A radar warning receiver.
AN/APR-44(V)3 radar warning receiver.
AN/AVR-2 laser detecting set.
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| More information on the OH-58D |
FAS - Military Analysis Network
www.army-technology.com
|