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KC-10A Extender

KC-10A Extender

Tanker Aircrafts
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Basic Information
Name
KC-10A Extender
Designation
KC-10A Extender
Alternate Designation
KDC-10 ARS
Equipment Type
Tanker Aircrafts
Manufacturer
Boeing
Date of Introduction
1981
Description

The KC-10A Extender is an advanced tanker and cargo aircraft designed to provide increased global mobility for US Armed Forces. It can transport up to 75 people and nearly 170,000 pounds of cargo a distance of about 4,400 miles unrefueled. The KC-10 has three large fuel tanks under the cargo floor as well as three main wing fuel tanks. Combined the 6 tanks carry more than 356,000 pounds of fuel, almost twice as much as the KC-135 Stratotanker. It uses an aerial refueling boom, or a hose and drogue centerline refueling system, to refuel a wide variety of military aircraft within the same mission. During refueling operations the fuel is transferred at a maximum rate of 1,100 gallons per minute using the boom, while the hose and drogue can refuel at a maximum rate of 470 gallons per minute. In addition, the KC-10 can be be in-flight refueled by another KC-10 or a KC-135 tanker aircraft to increase its delivery range. The KC-10 has a crew of 4 people: the pilot, copilot, flight engineer and boom operator. The KC-10A Extender is a derivative of commercial DC-10 aircraft and was deployed within the US Air Force in 1981. During operation Desert Shield in 1990 and Desert Storm in 1991, this aircraft provided in-flight refueling for US Air Force aircraft making possible the rapid deployment of US military forces to the Persian Gulf theater of operations. During the war the KC-10 and KC-135 tankers delivered about 125 million of gallons in 51,700 separate refueling operations.

Air & Air Defense Specifications
Crew 4
Max Speed 986.4 km/h
Range 7080.0 km
Service Ceiling 12800 m
Wingspan 50.00 m
Overview (Deagel)
Group Tanker Aircrafts
Status Active
Also Known As KDC-10 ARS
Origin United States of America
Contractor Boeing
Initial Operational Capability (IOC) 1981
Total Production 59
Unitary Cost USD $88 million
Specifications (Deagel)
Crew 4
Number of Engines 3
Dimensions — Height 17.4 meter
Dimensions — Length 54.4 meter
Dimensions — Wingspan 50 meter
Mass — Max Takeoff Thrust 157,500 pound
Mass — Max Takeoff Weight 268 ton
Mass — Payload 77,112 kilogram
Performance — Ceiling 12,800 meter
Performance — Max Range 7,080 kilometer
Speed — Top Speed at High Altitude 274 mps
Gear (Deagel)
Item 1 Turbofan Engines: F103 (3)
Details
Country of Origin United States
Category Aerial Refueling Aircraft
Air > Aerial Refueling Aircraft
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
54.4 m
Width
50 m
Height
17.4 m
Weight
268000 kg
Operators (2)
United States
Netherlands
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