Bell Helicopter - USA
Manufacturer(s)
United States (cancelled)
Operators
1998
Service Year
United States
National Origin
Cancelled
Project Status
0
(UNMANNED)
Crew
2
Units
UNMANNED
Aircraft inherently designed (or later developed) with an unmanned capability to cover a variety of over-battlefield roles.
18.2 ft
(5.56 meters)
Length
24.2 ft
(7.37 meters)
Width/Span
6.2 ft
(1.88 meters)
Height
1 x Pratt & Whitney Canada PW207D turboshaft engine delivering 641 horsepower each.
Propulsion
224 mph
(360 kph | 194 knots)
Max Speed
20,000 ft
(6,096 m | 4 miles)
Ceiling
MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
Up to 200lb of equipment or armament.