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TFX: by Digital Image Design

HUD (Heads Up Display) from TXX, 1993

F-22

SUPPLIER
Lockheed Advanced Development Company (LADC)

TYPE
Large, stealth-capable air superiority fighter
Secondary ground attack role

ENGINES
2 Pratt & Whitney F119-PW-100 Turbofans

SEA LEVEL RATED THRUST
155 kN (Afterburning)
111 kN (Military Power)

THRUST VECTORING
+/- 20 (Vertically)

DIMENSIONS
LENGTH
62.44 ft.

HEIGHT
16.5 ft.

WING AREA
842.4 sq. ft.

WING SPAN
44.75 ft.

TAILPLANE AREA
136.4 sq. ft.

FIN AREA
178.63 sq. ft.

WEIGHTS
OPERATING EMPTY
29,937.6 lbs.

MAX. TAKEOFF
59,875.2 lbs.

INTERNAL FUEL
21,953.8 lbs.

INTERNAL STORES
7,981.6 lbs.

ENVELOPE
MAX. LEVEL SPEED
Mach 2.30 (At Altitude)

SUPERCRUISE
Mach 1.58 (At Altitude)

TAKEOFF SPEED
135 knots *

LANDING SPEED
125 knots *

MAX. LANDING VSI
10 ft/s

TAKEOFF/LANDING RUN
3521 ft.

CRUISING SPEED
675 knots *

CRUISING ALTITUDE
59,000 ft *

COMBAT RADIUS
800 nm (nautical miles)

STALLING SPEED
95 knots (Sea Level)

MAX. AoA
22.50

G LIMIT
+9

* Own Estimates
NB: All above data refers to production land-based F-22A.

TFX PILOTS' NOTES

Landing gear is likely to be 'hard-wired' (manually controlled) as on the prototype. Handling will be 'carefree'. Effects of internal stores should be minimal, apart from increase in weight. "

From the manual