Everything about Xf-108 Rapier totally explained
The
North American XF-108 Rapier was a proposed
American design for a long-range, high-speed
interceptor aircraft to defend the
United States and
Canada from
supersonic Soviet bombers.
Development history
A very high performance, long-range interceptor had been proposed by the
USAF as early as
1952, but formal development of what became known as the
Long-Range Interceptor, Experimental (
LRI-X) wasn't approved until
20 July 1955. The specification was laid down on
6 October, calling for an aircraft that could fly at 60,000 ft (18,000 m) at a speed of Mach 1.7 (1,122 mph/1,795 km/h at that altitude) with a range of 1,150 miles (1,840 km). It was to have a two-man crew, at least two engines, and a powerful
radar. Contracts for preliminary studies were issued to
North American Aviation,
Lockheed, and
Northrop. Of the paper designs, the North American proposal, dubbed
NA-236, seemed most promising. Political and budgetary difficulties led to the cancellation of the program on
9 May 1956.
After considerable confusion, the program was reinstated on
11 April 1957 and North American was awarded a contract for two prototypes. The designation
F-108 was issued, also known as
Weapon System 202A. North American's company designation was
NA-257, although it was basically identical to NA-236. At the time,
Air Defense Command anticipated an order for 480 aircraft.
The resulting design went through considerable evolution, both owing to its cutting-edge technology and continual redefinition of the USAF requirements. In addition to the F-108's interceptor role, North American proposed it as an
escort fighter for the
Strategic Air Command's
XB-70 Valkyrie supersonic bomber, which NAA was also developing. The F-108 was intended to share the Valkyrie's
General Electric J93 engines and some other subsystems. By that time, however, it was unlikely that it would have served in that role. SAC had lost any interest in the escort fighter concept and, in any case, the F-108's range was at best marginal to accompany the B-70 all the way to its target and back.
Cancellation
The eventual design, which was built as a full-sized
XF-108 mock-up shown to Air Force officials in early
1959, was given the name "
Rapier" on
15 May 1959 following a contest by the
Air Defense Command asking airmen for suggestions. Production numbers were radically curtailed and the program was officially cancelled on
23 September of that year. North American kept refining the design through
1960 in hopes that the program might be revived, but it never was. Testing of the radar and missiles developed for the aircraft continued, intended for the
Lockheed YF-12 program, but that, too, was ultimately cancelled, and no Mach 3 interceptor has yet been operational in the U.S.
However, the money and time spent on the Rapier wasn't wholly in vain – the later
A-5 Vigilante supersonic bomber developed for the U.S. Navy retained the fuselage/weapon package and systems design of the Rapier. In many ways the Vigilante can be seen as the successful application of the Rapier design principles in a Mach 2 supersonic bomber design.
Design
The F-108 had a very large "cranked"
delta wing, with a 58° sweep angle at the leading edge and wingtip extensions of about 40°, with a 4°
anhedral. There were fixed ventral stabilizers on the wings, mounted at mid-span, and a tall all-moving vertical tailfin, supplemented by two ventral stabilizers that extended when the
landing gear retracted. Although some earlier versions of the design had had separate tailplanes and later forward
canards, both were abandoned in the final design. There were two
General Electric J93 turbojet engines, also used in North American's
XB-70 Valkyrie bomber, in the fuselage; USAF requests for an alternate installation of the
Pratt & Whitney J58 later used in the
SR-71 came to naught. The engines were fed by side-mounted intakes with a shape very similar to the later North American
A-5 Vigilante.
The large fuselage and wing had nine tanks for a total of 7,109 gallons (26,911 liters) of JP-6 fuel, giving an estimated combat radius of some 1,271 mi (2,033 km), which could be extended by
in-flight refueling. Top speed was estimated at 1,980 mph (3,190 km/h), about Mach 3, at 72,800 ft (22,200 m). It was stressed for +5.33/-3.00
g
.
The aircraft had a crew of two, a pilot and a weapon systems officer (WSO), in tandem cockpits. Each had an escape capsule designed to completely enclose each crewman in the event of emergency, permitting safe ejection even at extreme speeds and altitudes. The WSO in the rear seat had no flight controls.
The F-108 was intended to carry the
Hughes AN/ASG-18 radar, the
U.S.'s first
pulse doppler radar set. It was to have
look-down/shoot-down capability, but could only track one target at a time. It was a massive 2,100 lb (950 kg) installation filling most of the long nose. The radar was paired with an
infrared search and track (IRST) system with irdomes on the wing leading edges.
The radar was used to guide the
Hughes GAR-9 (later redesignated AIM-47)
air-to-air missile, three of which would be carried on a rotary launcher in an internal weapons bay. The GAR-9 was a very large, long-range weapon with its own radar set for terminal homing. It was intended to fly at Mach 6, with a range of almost 115 miles (185 km). An alternative version with a heat-seeking terminal homing mode was also developed. The missiles were 12 ft 6.5 in (3.82 m) long with a 33 in (84 cm) wingspan, weighing 818 lb (371 kg) for the radar version, 998 lb (453 kg) for the IR version. The earlier Northrop N-126 proposal suggested various weapons combinations, including
GAR-1 Falcon missiles, packs of 2.75 in (70 mm)
FFARs, or two
T-171 Vulcan 20 mm cannon, but none were part of the North American design.
The
F-111B and later
F-14 Tomcat would both adopt a pulse doppler radar and long range
AIM-54 Phoenix missiles similar to the AIM-47.
Specifications (XF-108, as designed)
|crew=2
|length main=89
ft 2
in
|length alt=27.2 m
|span main=57 ft 5 in
|span alt=17.5 m
|height main=22 ft 1 in
|height alt=6.7 m
|area main=1,865 ft²
|area alt=173.4 m²
|empty weight main=50,907
lb
|empty weight alt=23,098 kg
|loaded weight main=
|loaded weight alt=
|max takeoff weight main=102,533 lb
|max takeoff weight alt=46,508 kg
|engine (jet)=
General Electric YJ93-GE-3AR
|type of jet=
afterburning turbojet
|number of jets=2
|thrust main=20,900
lbf
|afterburning thrust main=29,300 lbf
|thrust alt=93.0 kN
|afterburning thrust alt=130.3 kN
|max speed main=1,980
mph
|max speed alt=1,720
kn, 3,190 km/h
|ceiling main=80,100 ft
|ceiling alt=24,400 m
|climb rate main=
|climb rate alt=
|range main=1,271
mi
|range alt=1,104
NM, 2,033 km
|range more=combat
|ferry range main=2,488 mi
|ferry range alt=2,162 NM, 4,004 km
|loading main=55.9 lb/ft²
|loading alt=183.4 kg/m²
|thrust/weight=0.56
|missiles=3×
Hughes GAR-9A
air-to-air missiles in an internal weapons bay
}}
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