Folland Fo.147

Swing-Wing Trainer / Light Strike Proposal [ 1961 ]

The Folland Fo.147 was proposed as an evolution of the Folland Gnat lightweight fighter-trainer with a built-in swing-wing capability.

Authored By: Staff Writer | Last Edited: 06/21/2019 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site.

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Into the 1960s, the British Royal Air Force (RAF) found itself in need of a budget-minded Advanced Jet Trainer (AJT) with inherent light strike capabilities. This led to a series of design brochures being published by the various British aero-industry players of the day. The Folland Fo.147 became a product of this period and held roots in the classic twin-seat, single-engine Folland "Gnat" fighter-trainer of 1959 (this aircraft is detailed elsewhere on this site). The Gnat found modest value on the global stage for its time, serving in the air forces of Britain, Finland, and India.

The Fo.147 was formed from the proposed supersonic, missile-armed, twin-seat, twin-engine Gnat Mk.5 fighter-trainer model. Key to Fo.147's design was integration of a "Variable Geometry" (VG) - or "swing wing" - capability in an effort to exact every ounce of speed and performance from the compact aircraft. Folland engineers believed that a VG arrangement in the Gnat could bring about speeds in excess of Mach 2 all the while retaining the proven inherent qualities of the existing aircraft - in this way, the revision would help increase all performance aspects of the original including operational range, straight-line speed, and operating ceiling.

Within the Fo.147 application, the wing sweep mechanism would allow the mainplanes to actively sweep (as needed) from an angle of 20 degrees to as much as 70 depending on the current flight phase - allowing the modified Gnat to operate equally-effectively at both low- and high-speed flying envelopes. Power would be provided through 2 x Rolls-Royce RB.153R series afterburning turbojet engines in a side-by-side arrangement within the body of the aircraft - these aspirated by side-fuselage intakes.

Another unique quality of the Fo.147 proposal, beyond its intended swing-wing capability, was the use of a rotating/retracting canard foreplane unit ahead of the cockpit section. This would take the place of any horizontal tailplanes in the design, leaving just the single vertical fin mounted aft of, and above, the engine installations.

A tandem, two-seat cockpit would feature pressurized workspaces for the crewmen and ejection seats were a must for enhanced survivability. Like the proposed Gnat Mk.5, the Fo.147 could be equipped with an Airborne Interception (AI) radar in the nose, most likely the Ferranti AI.23 series unit. Ground-running would be made possible by a retractable tricycle arrangement.

Dimensions included an overall length of 51 feet with a wingspan measuring 36.5 feet. Gross weight reached 18,500lb. With its engine pairing and unique wing arrangements, Folland engineers estimated their unique aircraft to have a maximum speed of Mach 2.2 with near-Mach 3 speeds deemed possible at some point.

While the Fo.147 and its related aircraft, the proposed Fo.148 featuring a more conventional tail unit, were ultimately abandoned, the requirement was eventually filled by the SEPECAT "Jaguar" (detailed elsewhere on this site). Beyond a single prototype, thirty-eight "Jaguar B" / Jaguar T.2 AJTs, offering an inherent secondary attack functionality, were taken into service.©MilitaryFactory.com

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Specifications

Service Year

1961

Origin

United Kingdom

Status

CANCELLED
Development Ended.

Crew

2

Production

0
UNITS

Folland Aircraft - UK

(View other Aviaton-Related Manufacturers)

United Kingdom (abandoned)

(OPERATORS list includes past, present, and future operators when applicable)

✓ Ground Attack (Bombing, Strafing)
Ability to conduct aerial bombing of ground targets by way of (but not limited to) guns, bombs, missiles, rockets, and the like.

✓ X-Plane (Developmental, Prototype, Technology Demonstrator)
Aircraft developed for the role of prototyping, technology demonstration, or research / data collection.

✓ Training (General)
Developed ability to be used as a dedicated trainer for student pilots (typically under the supervision of an instructor).

✓- Training (Advanced)
Dedicated advanced training platform for student pilots having graduated from basic flight training.

Length

51.0 ft
(15.55 m)

Width/Span

36.6 ft
(11.15 m)

Height

8.9 ft
(2.70 m)

Empty Wgt

14,110 lb
(6,400 kg)

MTOW

18,519 lb
(8,400 kg)

Wgt Diff

+4,409 lb
(+2,000 kg)

(Showcased structural values pertain to the base Folland Fo.147 production variant)

Installed: 2 x Rolls-Royce RB153R afterburning turbofan engines of unknown thrust output.

Max Speed

1,687 mph
(2,715 kph | 1,466 kts)

Ceiling

50,033 ft
(15,250 m | 9 mi)

Range

1,087 mi
(1,750 km | 3,241 nm)

Rate-of-Climb

20,250 ft/min
(6,172 m/min)

♦ MACH Regime (Sonic)

Sub

Trans

Super

Hyper

HiHyper

ReEntry

♦

(Showcased performance specifications pertain to the base Folland Fo.147 production variant. Performance specifications showcased above are subject to environmental factors as well as aircraft configuration. Estimates are made when Real Data not available. Compare this aircraft entry against any other in our database or View aircraft by powerplant type)

Assumed support for gun pods, rocket pods, and conventional drop bombs of the Cold War period.

Supported Types

Graphical image of an aircraft machine gun pod

Graphical image of aircraft aerial rockets

Graphical image of an aircraft rocket pod

Graphical image of an aircraft conventional drop bomb munition

(Not all ordnance types may be represented in the showcase above)

Hardpoint Mountings: 4

Fo.147 - Base Project Designation; cancelled.

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