AV-8B Harrier

Specifications
Contractor:	McDonnell Douglas Aircraft (Airframe Prime), Rolls Royce (Engine Prime)
Power Plant:	TAV-8B/AV-8B Day Attack (DA): One Rolls Royce Pegasus F402-RR-406 turbofan engine with approximately 20,280 pounds of thrust AV-8B Night Attack (NA)/AV-8B Radar: One Rolls Royce Pegasus F402-RR-408A turbofan engine with approximately 22,200 pounds of thrust
Accommodations:	AV-8B DA/NA/Radar Aircraft: Pilot only TAV-8B Trainer: Two seats
Performance:	Maximum airspeed: 550 KCAS Range greater than 142 nautical miles high speed/low altitude combat radius Maximum range: 900 nautical miles
Countermeasures:	Not applicable
Armament:	One fuselage-mounted 25 mm gun system Standard Air-to-Ground (A/G) load: Six Mk 82, 500 pound bombs Standard Air-to-Air (A/A) load: Four AIM-9L/M Sidewinder missiles Provisions for carrying up to 9,000 pounds of ordnance on seven stations
Mission and Capabilities:	The AV-8B single seat Vertical/Short Takeoff and Land (V/STOL) aircraft is the primary close air support/intermediate range intercept/attack mission fixed-wing aircraft for the USMC and the Spanish and Italian navies. The AV-8B can carry and deliver an assortment of conventional stores such as the Mk 83 1,000 pound GP bomb, GBU-12 500 pound LGB, GBU-16 1,000 LGB, CBU-99/100 Cluster Bomb Units, and 2.75" and 5" rockets. The NA configuration includes: night vision goggle-compatible cockpit controls and displays, a wide-field-of-view HUD, a Navigation Forward Looking Infrared (NAVFLIR) system, a Digital Map Unit (DMU), and an Angle Rate Bombing System (ARBS) with laser spot tracker, which provides first pass day or night target strike capability at low altitude/high speed. The Radar aircraft retains all night attack capability but integrates the AN/APG-65 radar system to extend the tracking capabilities of the aircraft for A/G delivery and A/A defense modes. V/STOL capability allows the AV-8B to be deployed with ground units using amphibious shipping and/or forward basing for rapid close air support response.
Program Summary:	All three variants of the AV-8B are in service with the USMC (deployed in WestPac and the Mediterranean). The Spanish Navy has DA/Radar AV-8Bs. The Italian Navy has Radar AV-8Bs only. The U.S., Italy, and Spain are partners in a collaborative international program. The original DA AV-8B was replaced by the NA variant in 1990, which incorporated the F402-RR-408A engine and expanded night fighting systems such as NAVFLIR, DMU, night vision goggle capability, and wide-field-of-view HUD. In 1993, the Radar AV-8B was fielded with the full night fighting capability and an AN/APG-65 Radar set to improve A/G and A/A tactical effectiveness. In 1994, the U.S. began a remanufacturing process to convert DA AV-8Bs to the Radar configuration (REMAN); deliveries began in 1996. Currently, a NA/Radar AV-8B upgrade program is underway to incorporate an Automatic Target Handoff System (ATHS) and Global Positioning System (GPS) capability into the aircraft. ATHS allows direct digital target/mission data exchange between the pilot and ground units. GPS integration improves navigational and weapons delivery accuracy. The AV-8B has seen service in the Persian Gulf (Desert Storm), Somalia (both U.S. and Italian AV-8Bs), and Bosnia (peacekeeping operations). A total of 51 Radar Aircraft are authorized for procurement by the U.S., Italy, and Spain. The U.S. has a planned procurement/delivery program for 73 REMAN AV-8Bs (FY 1996 - 2002).

External Dimensions:

Wing Span	9.25 m
Length overall (flying attitude)
AV-8B	14.12 m
TAV-8B	15.32 m
GR. Mks 5/7	14.36 m
T. Mk 10	15.79 m
Height overall	3.55 m
Tailplane span	4.24 m
Outrigger wheel track	5.18 m

Areas
Wings, excl LERX, gross	21.37 m²
LERX (total): Pegasus 11-21	0.81 m²
Pegasus 11-61	1.24 m²
100 percent	1.39 m²
Ailerons (total)	1.15 m²
Trailing-edge flaps (total)	2.88 m²
Ventral fixed strakes (total)	0.51 m²
Ventral retractable fence (LIDs)	0.24 m²
Ventral airbrake	0.42 m²
Fin	2.47 m²
Rudder, excl tab	0.49 m²
Tailplane	4.51 m²

Weights and Loadings (Single-Seaters, Except Where Indicated)

Operating weight empty (including pilot and used fuel)
AV-8B	6,336 kg
GR. Mk 7	7,050 kg
TAV-8B	6,451kg
Maximum fuel
Internal only	3,519 kg
Internal and external	7,180 kg
Maximum external stores
Pegasus 11-61	6,003 kg
Pegasus 11-21/Mk 105*	4,899 kg
Maximum useful load (include fuel, stores, weapons, ammunition and water injection for engine)
Vertical takeoff	Approximately 3,062, kg
STO	More than 7,710 kg
Basic flight design gross weight for 7g operation	10,410 kg
Maximum T-O weight
435 meters STO	14,061 kg
S/L VTO, ISA:
AV-8B/Pegasus 11-61	9,342 kg
GR. Mk 7	8,700 kg
S/L VTO, 32°C	8,142 kg
Design maximum landing weight	11,340 kg
Maximum vertical landing weight	9,043 kg 205 kg less in TAV-8B

Performance

Maximum mach number in level flight
At S/L	875 knots
At altitude	0.98
STOL takeoff run at maximum takeoff weight:
ISA	435 m
At 32° c	518 m
Operational radius with external loads shown:
Short takeoff (366 m, 12 Mk 82 Snakeye Bombs, internal fuel, 1 hour loiter)	90 nautical miles
Hi-lo-hi, short take off (366 m, seven Mk 82 Snakeye Bombs, two 300 US gallon external fuel tanks no loiter	594 nautical miles
Deck launch intercept mission, two AIM-9 missiles and two external fuel tanks	627 nautical miles
Unrefueled ferry range
Tanks dropped	1,965 nautical miles
Tanks retained	1,638 nautical miles
Combat air patrol endurance at 100 nautical miles from base.	3 hr.
"G" force limits	+8/-3

CHARACTERISTIC	RADAR	NIGHT ATTACK	DAY ATTACK
Aircraft Length (feet)	47.75	46.33	46.33
Aircraft Height (feet)	11.66	11.66	11.66
Aircraft Wingspan (feet)	30.35	30.35	30.35
Operating Weight Empty (pounds)	14,912	13,968	13,705
Maximum Vertical Takeoff Weight (pounds)	20,752	20,752	19,185
Maximum Short Takeoff Weight (pounds)	32,000	32,000	31,000
Internal Fuel Weight (pounds)	7,762	7,762	7,762
Maximum External Fuel Weight (pounds)	8,073	8,073	8,073

NEWSLETTER

Join the GlobalSecurity.org mailing list

Military

AV-8B Harrier

External Dimensions:

Areas

Weights and Loadings (Single-Seaters, Except Where Indicated)

Performance