| . |
**Data for each of these
characteristics can be
obtained by contacting
the EICO
Aviation Specialist
at the NAVFAC Criteria
Office.
|
 The
Boeing X-32 JSF short takeoff and vertical landing (STOVL) variant for
the U.S. Marine Corps and U.K. Royal Navy employs a direct lift system
for short takeoffs and vertical landings with uncompromised up-and-away
performance.
|
|
Aircraft Type |
Fighter
|
|
Aircraft Manufacturer
|
Boeing
|
Engine Manufacturer |
Pratt
& Whitney
|
Engine Number |
F119-PW-100
|
Type of Landing Gear |
Single Tricycle
|
Design Gear Load |
|
Design Tire Pressure |
|
Pass/Cov Ratio Channelized |
|
|
Pass/Cov Ratio Unchannelized
|
|
|
|
Wingspan |
30 ft
|
Length (Overall) |
46 ft
|
Height (Overall) |
13.3 ft
|
Wheelbase |
|
Nose to centerline of main gear |
|
|
Wheel track (tread) Main
|
|
|
Wheel track (tread) Nose
|
|
Vertical clearance of wingtip at
maximum weight |
|
Centerline of fuselage to
approximate pivot point based on maximum
steering angle or locked wheels |
|
Height of jet engine on
centerline of fuselage |
|
|
|
Minimum turning radius |
|
Engine operating danger areas -
idle |
|
Ground clearance |
**
|
Electrical Service |
• Maximum kVa by aircraft
for 400Hz distribution |
|
Mechanical Service |
• Air starting system |
|
• Preconditioned air |
|
• Environmental control air |
|
|
|
Min takeoff weight |
22,000 lbs
|
Min takeoff distance with min
takeoff weight |
|
Min takeoff distance with min
takeoff weight with abort distance |
**
|
Max takeoff weight at peace-time |
50,000 lbs
|
Max takeoff weight at war-time |
50,000 lbs
|
Min takeoff distance with max
takeoff weight |
|
Min landing weight |
|
Max landing weight |
|
• Corner |
|
• Field |
|
|
Peace-time weight used for pavement evaluation
|
|
• Min landing distance at min landing
weight
|
|
|
• Min landing distance at max landing
weight
|
|
View / Sort aircraft on Spreadsheet.
|
