SPECIFICATIONS

F-22A TACTICAL DATA PACKAGE

Complete technical specifications derived from USAF fact sheets, manufacturer data, and open-source intelligence. All values represent Block 30/35 production configuration unless noted.

CREW

1

SINGLE PILOT

GEN-01

LENGTH

62' 1"

18.92 M

OVERALL FUSELAGE LENGTH

GEN-02

WINGSPAN

44' 6"

13.56 M

TIP TO TIP

GEN-03

HEIGHT

16' 8"

5.08 M

TOP OF VERTICAL STABILIZERS

GEN-04

WING AREA

840 SQ FT

78.04 M²

REFERENCE AREA

GEN-05

ASPECT RATIO

2.36

WINGSPAN² / WING AREA

GEN-06

AIRFOIL

NACA 6 SERIES

MODIFIED FOR STEALTH

GEN-07

EMPTY WEIGHT

43,340 LB

19,700 KG

NO FUEL / NO WEAPONS

GEN-08

GROSS WEIGHT

64,840 LB

29,410 KG

50% FUEL / A/A LOAD

GEN-09

MAX TAKEOFF

83,500 LB

38,000 KG

MAXIMUM ALLOWABLE

GEN-10

FUEL (INTERNAL)

18,000 LB

8,200 KG

JP-8 / INTERNAL TANKS

GEN-11

FUEL (W/ TANKS)

26,000 LB

12,000 KG

+ 2× 600 US GAL EXTERNAL

GEN-12

GENERAL CHARACTERISTICS

CREW1
LENGTH62' 1"
WINGSPAN44' 6"
HEIGHT16' 8"
WING AREA840 SQ FT
ASPECT RATIO2.36
AIRFOILNACA 6 SERIES
EMPTY WEIGHT43,340 LB
GROSS WEIGHT64,840 LB
MAX TAKEOFF83,500 LB
FUEL (INTERNAL)18,000 LB
FUEL (W/ TANKS)26,000 LB

12 PARAMETERS LOADED

VIEW DESIGN PHILOSOPHY

DATA SOURCES

  • ▸USAF F-22A Fact Sheet (Official)
  • ▸Lockheed Martin Aeronautics Data
  • ▸Boeing Defense, Space & Security
  • ▸Pratt & Whitney F119 Specifications
  • ▸Aviation Week & Space Technology
  • ▸Air Forces Monthly
  • ▸Journal of Electronic Defense
  • ▸Aerofax: Lockheed Martin F-22 Raptor
  • ▸Code One Magazine (Lockheed Martin)
  • ▸Flight International
  • ▸Jane's All the World's Aircraft

CLASSIFICATION NOTICE

This compilation derives from unclassified open-source intelligence. Actual operational parameters remain classified. Values represent best available public data as of 2024.

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