MAIN FEATURES
Arrestor hook (lowered)
Outward retracting, single
wheel main gear unit
Xar IFR receptacle (open)
Forward retracting,
steer-by-wire single
wheel nose gear
Auxiliary blow-in doors
(open – taxi)
Vectorable exhaust nozzle in 20º
(fully extended) position. Also acts
as a flight control surface/airbrake
Auxiliary blow-in
doors (open – taxi)
F-22A (armed and dirty)
Ventral missile bay
door (open)
AN/APG-77
ASEA radar
M61A2 six-barrelled 20 mm cannon
Datalink antenna
Missile launch detector
GPS
antenna
CNI UHF
antenna
L-band antenna
Countermeasures
dispenser bay
Lateral missile bay open, LAU-141/A
trapeze launch rail extended
GEC-Marconi
wide-angle HUD
Avionics: Lear Astronics VMS
(Vehicle Management System)
and IVSC (Integrated Vehicle
Subsystem Control), TRW CNI
(Comms/Nav/ID) systems,
Sanders AN/ALR-94 RWR/ESM,
Litton LN-100G laser gyros,
fibre optic data bus
Ventral missile bays with LAU-142/A
trapeze launch rails (open)
External store wing mounts
F-22A (armed)
Ventral missile bays
Wingtip formation light
Arrestor hook
M61A2 six-barrelled
20 mm cannon
Inlet bleed air duct/
door/spoiler panel
Lateral missile bay
Outward-canted tail unit
due to RCS rquirements
Frameless, multiple laminated canopy with
layer to minimise radar return, hinged at rear
Pitot head
Countermeasures
dispenser bay
Auxiliary blow-in doors
Angular nose/intake shape for low RCS
Vectorable exhaust nozzle – also acts
as a flight control
surface/airbrake
Pratt and Whitney F-119-PW-100 thrust vectored turbofans
Shoulder mounted wing with 42º leading
edge sweep and 'complex camber'
All-moving tailplane
McDonnell Douglas
ACES II zero-zero
ejector seat
Radome with static
electricity 'zipper' strips
Large,
forward
-set tail
Leading edge flaps
Tailing edge aileron/flaperon
F-22A (clean)
F-22 RAPTOR: 2
ILLUSTRATIONS: © ADRIAN DAVID MOORE 2015 • NO ITEMS MAY BE REPRODUCED WITHOUT THE PERMISSION OF THE COPYRIGHT HOLDER
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ILLUSTRATIONS: © ADRIAN DAVID MOORE 2015
