Lockheed Martin - USA
Manufacturer(s)
United States (possible)
Operators
2027
Service Year
United States
National Origin
In-Development
Project Status
6
Crew
0
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).
MARITIME / NAVY
Land-based or shipborne capability for operating over-water in various maritime-related roles while supported by allied naval surface elements.
TRANSPORT
General transport functionality to move supplies/cargo or personnel (including wounded and VIP) over range.
SPECOPS
Serving Special Forces / Special Operations elements and missions.
MULTI-ENGINE
Incorporates two or more engines, enhancing survivability and / or performance.
RUGGED AIRFRAME
Inherent ability of airframe to take considerable damage.
EXTENDED RANGE PERFORMANCE
Capability to travel considerable distances through onboard fuel stores.
MARITIME OPERATION
Ability to operate over ocean in addition to surviving the special rigors of the maritime environment.
CREWSPACE PRESSURIZATION
Supports pressurization required at higher operating altitudes for crew survival.
ENCLOSED CREWSPACE(S)
Features partially- or wholly-enclosed crew workspaces.
RETRACTABLE UNDERCARRIAGE
Features retracting / retractable undercarriage to preserve aerodynamic efficiency.
ENHANCED ACCESS
Design incorporates feature(s) that facilitates loading / unloading of cargo / personnel from the aircraft.
97.8 ft
(29.80 meters)
Length
132.5 ft
(40.40 meters)
Width/Span
54.3 ft
(16.55 meters)
Height
78,044 lb
(35,400 kilograms)
Empty Weight
166,449 lb
(75,500 kilograms)
Maximum Take-Off Weight
+88,405 lb
(+40,100 kg)
Weight Difference
monoplane / high-mounted / straight
Mainplane Arrangement
Monoplane
Design utilizes a single primary wing mainplane; this represents the most popular modern mainplane arrangement.
High-Mounted
Mainplanes are mounted at the upper-most position allowable along the dorsal line of the fuselage.
Straight
The planform involves use of basic, straight mainplane members.
4 x Rolls-Royce AE2100D3 turboprop engines developing 4,637 horsepower each driving six-bladed propeller units.
Propulsion
407 mph
(655 kph | 354 knots)
Max Speed
27,887 ft
(8,500 m | 5 miles)
Ceiling
2,209 miles
(3,555 km | 1,920 nm)
Range
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
