| . |





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

The
Osprey is a tilt-rotor aircraft with a 38-foot rotor system and engine/transmission
nacelle mounted on each wing tip. It can operate as a helicopter when
taking off and landing vertically. Once airborne, the nacelles rotate
forward 90 degrees for horizontal flight, converting the V-22 to a high
speed, fuel-efficient turboprop airplane. The wing rotates for compact
storage aboard ship. The first flight occurred in March 1989. The Navy's
HV-22A will provide combat search and rescue, delivery and retrieval
of special warfare teams along with fleet logistic support transport.
The Marine Corps' MV-22A will be an assault transport for troops, equipment,
and supplies, operating from air capable ships or bases ashore.
|
|
Aircraft Type |
Transport
(VTOL) |
|
Aircraft Manufacturer
|
Bell-Boeing
|
Engine Manufacturer |
Bell-Boeing
|
Engine Number |
T406-80-400 |
Type of Landing Gear |
Dual Tricycle |
Design Gear Load |
11,195 lbs. |
|
|
Wingspan (Folded) |
84.63 ft (18.42 ft) |
Length Overall |
62.27 ft |
Height Overall (Folded) |
22.11 ft (18.1 ft) |
Wheelbase |
25.02 ft |
Nose to centerline of main gear |
** |
Wheel track (tread) |
13.00 ft |
Vertical clearance of outboard
engine at maximum weight |
4.64 ft |
Vertical clearance of wingtip at
maximum weight |
** |
|
|
Minimum turning radius |
** |
Engine operating danger areas |
** |
Ground clearance |
** |
Electrical Service |
Maximum kVa by aircraft
for 400Hz distribution |
37 kVa |
Mechanical Service |
Air starting system |
** |
Preconditioned air |
** |
Environmental control air |
** |
|
|
Min takeoff weight |
37.93 klbs |
Min takeoff distance with min
takeoff weight |
2,900 ft |
Min takeoff distance with min
takeoff weight with abort distance |
** |
Max takeoff weight at peace-time |
60.50 klbs |
Max takeoff weight at war-time |
60.50 klbs |
Min takeoff distance with max takeoff weight with abort distance |
3,400 ft |
Min landing weight |
35.31 klbs |
Max landing weight |
60.50 klbs |
Min landing distance at min
landing weight |
** |
Min landing distance at max
landing weight |
** |
Peace-time weight used for
pavement evaluation |
** |
View / Sort aircraft on Spreadsheet.
|