Bell 360 Invictus

Future helicopter Derived from 525 Relentless
2022





Model



Bell 360 Invictus

Bell proposal for US Army Future Attack Reconnaissance Aircraft FARA programme.

The Bell Invictus features a tandem cockpit, an enclosed canted tail rotor and will be powered by two GE Aviation T901 engines along a supplemental power unit




Model News


Triumph to Supply Bell 360 Subsystems, 28-May-20 : #Triumph Triumph Group will supply hydraulic pump and reservoir assemblies based on those for the Bell 525 Relentless to Bell for the Bell 360 competitive prototype demonstrator in the US Army Future Attack and Reconnaissance Aircraft (FARA) competition

Manufacturing Evolution at Bell Helicopters, 03-Apr-20 : #manufacturing Bell produced 150 UH-1 Hueys per month in addition to 50 other helicopters in its peak production period during the Vietnam War. Now the factory is getting prepared for US Army’s Future Vertical Lift FLRAA and FARA programs and pave the way for urban air mobility aircraft

Bell 360 Selected to Continue in FARA Competition, 31-Mar-20 : #FARA Bell selected to continue work on the Bell 360 Invictus as part of the US Army Future Attack Reconnaissance Aircraft (FARA) program

Bell 360 Invictus Announced for US Army FARA, 02-Oct-19 : #Invictus Bell unveiled its Bell 360 Invictus proposal for the US Army’ Future Attack Reconnaissance Aircraft (FARA) competition. Based on Bell 525 new technologies, the 360 will offer a 135 nm ~ 250 km combat radius with speeds in excess of 200 Knots ~ 370 km/h



Specifications


Engine: 2 x GE T901 3000 shp
Capacity:
Length: (m)
Height: (m)
Blades:
Rotor diam.: (m)
Disc area: (m2)
Weight: (kgs)
Speed: (km/h)
Range: (km)
Ceiling: (m)
Rate/Climb: (m/min)
blueprints


List of Operators of Bell 360 Invictus


From Organisation with model 360 Invictus



Construction Numbers on database of 360 Invictus or its versions

1360 Invictus




Construction Numbers

Help Us

C/NBuilt asYearHistory
mockup US mockup : Bell 360 Invictus Mockup for FARA program; 15oct19 pict+


1 C/N.


share     facebook     twitter     linkedin