General Dynamics F-111 Aardvark

Long-Range Strategic Medium Bomber / Tactical Strike Aircraft

United States | 1967

"The General Dynamics F-111 Aardvark swing-wing bomber was retired in 1996 from active service with the United States Air Force followed shortly by its counterpart - the EF-111 Raven."

Authored By: Staff Writer | Last Edited: 05/31/2024 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site; No A.I. was used in the generation of this content.

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The General Dynamics F-111 "Aardvark" was purposely-designed as a variable geometry "swing wing" platform from the outset. The variable swing-wing philosophy would allow the aircraft to utilize three pre-determined geometric wing positions that could be called upon to change the flight characteristics of the aircraft "on the fly". The first position, with wings fully extended, was to be used when the increased weight of the aircraft - due to ordnance and/or fuel - could produce additional drag properties under the wing, assisting the aircraft on take-off. The secondary position could be utilized to attain stability and speed at high subsonic speeds. The third position, with wings completely swept back against the fuselage, could be utilized for maximum "fast-dash" performance at altitude.

The F-111 was based on this design principle, becoming the world's first operational variable geometry swing wing aircraft - leading the way for future global counterparts in the form of the Grumman F-14 Tomcat interceptor, the Panavia Tornado multirole aircraft, the Mikoyan-Gurevich MiG-23 and MiG-27 "Flogger" strike fighters and the Sukhoi Su-17 "Fitter" bombers. Additionally, larger (and more complex) forms of the swing-wing philosophy would also arise from the developments of the Rockwell B-1 "Lancer", the Tupolev Tu-22 "Backfire" and the Tupolev Tu-160 "Blackjack" bombers.

The F-111 (belatedly assigned the designator of "Aardvark") was a large two-seat multi-role aircraft that would be used to good effect in the upcoming Vietnam War. The two crew members sat in a side-by-side arrangement in a fully-jettisonable cockpit capsule, with each member having equal access to all controls on the main panel. The F-111 was powered by a series of ever-increasing Pratt & Whitney brand powerplants and could field a variety of laser-guided, seeking, and drop bombs from up to 8 underwing hardpoints (four to a wing - the area under the fuselage was reserved for an internal weapons bay though the area between the engines could fit an ECM or data link pod). The aircraft utilized a single vertical tail fin mounted between the twin engines running that ran aft of the cockpit and the remaining length of the fuselage.

Early development of the F-111 proved problematic and costly. The fleet defense derivative which was designated the F-111B for the US Navy was cancelled altogether due to performance and weight issues (the latter issue directly related to the former). Even when the system was already in operational status along the frontlines over Vietnam, the system was still exhibiting technological issues. Despite these initial shortcomings, the product evolved into an effective and multi-faceted combat platform that would see service up until the late 1990's.

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The F-111C became an export model to the only other operator of the F-111, that being Australia. Delivery of these 24 aircraft were delayed until 1973 when they had been originally ordered as early as 1963. Four of these became hybrid reconnaissance/bomber models as RF-111Cs, fitted with cameras and reconnaissance equipment while still retaining their combat strike capabilities.

The F-111D was an "improved" Aardvark featuring uprated engines, new avionics, a revised canopy and a revised air intake. Ninety-Six were delivered with operational service attained in 1974. Delayed once again hampered these deliveries, for the D-models were ordered several years prior in 1967. The F-111E became an interim model following the "breaking-in" issues encountered with the D-models. Ninety-four of these E-models arrived even before the D-models were brought fully online.

F-111F was the final production variant of the Aardvark line. Improved avionics, simplified systems and improved capabilities stemmed from this new model. The FB-111A "Switchblade" (name is unofficial) was a strategic bomb variant used in place of Boeing B-52 Stratofortresses and Convair B-58 Hustlers in service with US Strategic Air Command. Production of this type amounted to 76 examples. The F-111K was a British order intended to fill the void of the cancelled BAC TSR-2 bomber program fro 1965, with the Aardvark order itself eventually canceled by the British in 1968. The F-111G were used as trainers.

The evolution of the F-111 saw the aircraft pass through a series of first-run models that focused on increasing the performance of the Pratt & Whitney engines. Forty-two F-111A models were also converted to the famous EF-111 Raven series of electronic warfare aircraft (conversions completed by Grumman) and were utilized in the Persian Gulf War. These systems were originally designed to replace the aging Douglas EB-66 aircraft. The Raven models featured a noticeable bulb on the top of their vertical tail fins.

The US Strategic Air Command (SAC) operated their FB-111 models from 1969 through 1990 while the USAF usage covered 1967 through 1998 (the USAF batch consisting of Ravens).

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Cockpit
While traditional jobs involve workstations, office desks, or cubicles, aircraft provide operators with their own unique, ever-changing view of the world below.

[ Click to Enlarge ]

Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the General Dynamics F-111F Aardvark Long-Range Strategic Medium Bomber / Tactical Strike Aircraft.

2 x Pratt & Whitney TF30-P-111 turbofan engines developing 25,100 lb of standard thrust each.
Propulsion

1,650 mph
2,655 kph | 1,434 kts
Max Speed

65,945 ft
20,100 m | 12 miles
Service Ceiling

4,200 miles
6,760 km | 3,650 nm
Operational Range

25,890 ft/min
7,891 m/min
Rate-of-Climb

City-to-City Ranges
Operational range when compared to distances between major cities (in KM).

NYC

LON

PAR

BER

MOS

TOK

SYD

LAX

NYC

Structure
The nose-to-tail, wingtip-to-wingtip physical qualities of the General Dynamics F-111F Aardvark Long-Range Strategic Medium Bomber / Tactical Strike Aircraft.

2
(MANNED)
Crew

73.5 ft
22.40 m
O/A Length

63.0 ft
(19.20 m)
O/A Width

17.1 ft
(5.22 m)
O/A Height

47,179 lb
(21,400 kg)
Empty Weight

100,002 lb
(45,360 kg)
MTOW

Design Balance
The three qualities reflected below are altitude, speed, and range. The more full the box, the more balanced the design.

RANGE

ALT

SPEED

Armament
Available supported armament and special-mission equipment featured in the design of the General Dynamics F-111 Aardvark Long-Range Strategic Medium Bomber / Tactical Strike Aircraft provided across 9 hardpoints.

OPTIONAL:
1 x 20mm M61 Vulcan internal cannon.

Mission-specific ordnance can include any of the following (up to 31,500lb):

GBU-12 laser-guided bomb.
GBU-10 laser-guided bomb.
AGM-84 HARM anti-radar anti-radiation Missile.
GBU-15b bomb.
AGM-142 air-to-surface missile.
AIM-9 "Sidewinder" air-to-air missile.
Conventional Iron / Dumb / Drop Bombs.

X X X

X

Hardpoints Key:

Centerline

Wingroot(L)

Wingroot(R)

Wing

Wingtip

Internal

Not Used

Variants
Notable series variants as part of the General Dynamics F-111 Aardvark family line.

F-111A - Initial Production Model Designation; 23 pre-production models produced; Total of 158 at production end fitted with 18,500lb TF30-P-3 powerplants; 42 converted to EF-111A Ravens.

F-111B - Cancelled Fleet Defense Variant of which 5 pre-production models were produced.

F-111C - Australian Export Models of which 24 were produced.

F-111D - 96 Production Models fitted with TF30-P-0 powerplants generating 19,600lbs of thrust each.

F-111E - 94 Production Models of this type; developed as an interim to the F-111D model.

F-111F - 106 Production Models of this type fitted with TF30-P-111 capable of 25,100lbs of thrust each.

F-111G - Converted FB-111A Models for European Theater use; RAAF usage of this model as well.

F-111K - Proposed British export model with British equipment; order eventually cancelled.

FB-111A - Strategic Bomber Model Designation; 76 examples produced; fitted with 2 x additional hardpoints, increased wingspan and TF30-P-7 powerplants generating 20,150lbs of thrust; improved electronics.

EF-111A "Raven" - Electronic Warfare Conversion Models of F-111A series; 42 converted in this way; last to be retired from USAF use in 1998.

Operators
Global customers who have evaluated and/or operated the General Dynamics F-111 Aardvark. Nations are displayed by flag, each linked to their respective national aircraft listing.

Total Production: 554 Units
Contractor(s): General Dynamics - USA

[ Australia; United States ]

Relative Max Speed

Hi: 1700mph

Lo: 850mph

Aircraft Max Listed Speed (1,650mph).

Graph Average of 1,275 MPH.

Era Crossover

Showcasing Aircraft Era Crossover (if any)

Max Alt Visualization

Production Comparison

554

36183

44000

Entry compared against Ilyushin IL-2 (military) and Cessna 172 (civilian) total production.

MACH Regime (Sonic)

Sub

Trans

Super

Hyper

HiHyper

ReEntry

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