Brantly Helicopter Corporation (Brantly International, Incorporated) - USA
Manufacturer(s)
China; United States
Operators
1958
Service Year
United States
National Origin
Active
Project Status
1
Crew
334
Units
SPECIAL-MISSION: MECICAL EVACUATION
Extraction of wounded combat or civilian elements by way of specialized onboard equipment and available internal volume or external carrying capability.
SPECIAL-MISSION: SEARCH & RESCUE
Ability to locate and extract personnel from areas of potential harm or peril (i.e. downed airmen in the sea).
INTELLIGENCE-SURVEILLANCE-RECONNAISSANCE
Surveil ground targets / target areas to assess environmental threat levels, enemy strength, or enemy movement.
UNMANNED
Aircraft inherently designed (or later developed) with an unmanned capability to cover a variety of over-battlefield roles.
27.6 ft
(8.40 meters)
Length
23.8 ft
(7.25 meters)
Width/Span
6.9 ft
(2.10 meters)
Height
1,025 lb
(465 kilograms)
Empty Weight
1,676 lb
(760 kilograms)
Maximum Take-Off Weight
+650 lb
(+295 kg)
Weight Difference
1 x Avco Lycoming IVO-360-A1A air-cooled piston engine developing 180 horsepower and driving three-bladed main rotor and two-bladed tail rotor.
Propulsion
99 mph
(160 kph | 86 knots)
Max Speed
10,827 ft
(3,300 m | 2 miles)
Ceiling
249 miles
(400 km | 216 nm)
Range
1,900 ft/min
(579 m/min)
Rate-of-Climb
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