| . |

 


**Data for each of these
characteristics can be
obtained by contacting
the EICO
Aviation Specialist
at the NAVFAC Criteria
Office.
|

The
KC-135 Stratotanker's principal mission is air refueling. This asset
greatly enhances the U. S. Air Force's capability to accomplish its
mission of Global Engagement. It also provides aerial refueling support
to U.S. Navy, U.S. Marine Corps and allied aircraft. Four turbofans,
mounted under 35-degree swept wings, power the KC-135 to takeoffs at
gross weights up to 322,500 pounds (146,285 kilograms). Nearly all internal
fuel can be pumped through the tanker's flying boom, the KC-135's primary
fuel transfer method. A special shuttlecock-shaped drogue, attached
to and trailed behind the flying boom, may be used to refuel aircraft
fitted with probes. An operator stationed in the rear of the plane controls
the boom. A cargo deck above the refueling system can hold a mixed load
of passengers and cargo. Depending on fuel storage configuration, the
KC-135 can carry up to 83,000 pounds (37,648 kilograms) of cargo.
|
|
Aircraft Type |
Support |
|
Aircraft Manufacturer
|
Boeing
|
Engine Manufacturer |
CFM
|
Engine Number |
F108-CF-100
|
Type of Landing Gear |
Dual Tandem Tricycle |
Design Gear Load |
142,000 psi |
Design Tire Pressure |
155 psi |
Pass/Cov Ratio Channelized |
3.37 |
Pass/Cov Ratio Unchannelized |
5.97 |
|
|
Wingspan |
130.80 ft |
Length (Overall) |
136 ft 3 in"
|
Height (Overall) |
38 ft 4 in"
|
Wheelbase |
59 ft |
Nose to centerline of main gear |
708.00 ft |
Wheel track (tread) |
22.08 ft |
|
|
Minimum turning radius |
** |
Engine operating danger areas |
** |
Ground clearance |
** |
Electrical Service |
Maximum kVa by aircraft
for 400Hz distribution |
** |
Mechanical Service |
Air starting system |
** |
Preconditioned air |
** |
Environmental control air |
** |
|
|
Min takeoff weight |
240 klbs |
Min takeoff distance with min
takeoff weight |
** |
Min takeoff distance with min
takeoff weight with abort distance |
** |
Max takeoff weight at peace-time |
301.6 klbs |
Max takeoff weight at war-time |
322.5 klbs |
min takeoff distance with max
takeoff weight |
** |
Min landing weight |
** |
Max landing weight |
322.5 klbs |
Min landing distance at min
landing weight |
** |
Min landing distance at max
landing weight |
** |
Peace-time weight used for
pavement evaluation |
** |
|