Notes: This was
one the first British jet carrier aircraft, and were designed specifically to
oppose the Soviet Sverdlov class of light cruisers.
The Buccaneer’s first flight was in 1958, and it entered service with the
Royal Naby in 1962. When the Buccaneer was designed, it was one of the very few
strike aircraft able to attack in the clean configuration, due to its internal
weapons bay. When Britain went to the smaller carriers with Harriers, the
Buccaneers were relegated to land bases, usually as anti-ship planes, and then
were eventually phased out. They
were also operated by South Africa, usually in the long-range strike role, but
were also phased out by that country.
The Buccaneer has an internal bomb bay, unusual for an aircraft of its
size; this bay can hold 1.81 tons or 2040 liters of fuel.
The aircraft has ejection seats and is capable of in-flight refueling.
The Buccaneer is capable of nuclear weapons delivery. The Buccaneer’s aviators
and crews affectionately call the Buccaneer the “Banana Jet” due to the type’s
developmental name, the BANA (Blackburn Advanced Naval Aircraft).
The Buccaneer is
sort of wedge-shaped, with bulbous air intakes and large, round engine fairings.
It has a T-tail and medium-length wings. The Buccaneer is designed for a
supersonic low-level dash to its target (it is capable of Mach 1.2 at sea
level), and a supersonic high flight if necessary. It did not see combat service
in the Royal Navy but did with the Royal Air Force during the Gulf War, and had
combat service as a strike and interdiction aircraft with the South African Air
Force. Blackburn was not able to make weapon bay doors that were stable in the
low-level high speed run up to the target that the designers envisioned, so
Blackburn came up with a rotating bomb release mechanism which turned around the
axis of the weapons bay and exposed the stores in the weapons bay to the
slipstream, at which point they could be released, singly or all at once. (The
original envisioned weapon to put in the bay was the 900-kilogram Red Beard
20-kiloton nuclear bomb.)
Buccaneer S.1/S.2
The Buccaneer
S.1 designation applied to the initial prototypes and a handful of production
examples. These were found wanting
in their short service due to their underpowered de Havilland Gyron Junior
engines, with the pair fitted to the S.1 developing 14,200 pounds thrust, much
too low for the weight and requirements of the aircraft. To land on board an
aircraft carrier, the Buccaneer was dependent on using blown flaps, and the lack
of adequate engine power would make the blown flap system fail as the worst
moment, leading to a sudden stall as it was about to set down on the deck. They
were replaced quickly by the S.2, but eight S.1s saw continued service as
Buccaneer aircrew training aircraft until 1970.
The S.2 differs
from the S.1 in being powered by an iteration of the Rolls Royce Spey turbofan,
which has 40% more thrust and much less fuel consumption, due to the Spey being
a turbofan and not a turbojet like the Gyron Junior.
The Buccaneers That
Never Were…
After Hawker
Siddeley acquired Blackburn, they put forward some proposed updates and changes
to the Buccaneer, largely by incorporating avionics from the cancelled TSR.2.
Two ideas were put forward: the upgraded S.2*, and the further-upgraded
S.2**. (It is probable that if they had been adopted, they would have been
designated the S.3 and possibly S.4.) Changes may be seen in the tables below.
Hawker stated that they could supply an aircraft with the same capabilities as
the F-111K but at half the cost. In
the end, however, neither the TSR.2, F-111K, nor the upgraded Buccaneers were
proceeded with.
Twilight 2000
v2.2 Notes: Buccaneers were also used against land targets in the Twilight War,
though by that war they were largely replaced by Tornadoes and were operated
only in a secondary role or to replace Tornado losses.
South Africa also used some of these aircraft in the Twilight War.
|
Aircraft |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
Buccaneer S.1 |
$22,619,513 |
JP8 |
7.26 tons |
28.12 tons |
2 |
19 |
Radar (90 km), FLIR (12 km) |
Shielded |
|
Buccaneer S.2 |
$24,000,768 |
JP8 |
7.26 tons |
28.65 tons |
2 |
19 |
Radar (90 km), FLIR (12 km) |
Shielded |
|
Buccaneer S.2* |
$29,663,490 |
JP8 |
7.26 tons |
28.8 tons |
2 |
19 |
Radar (120 km), FLIR (12 km) |
Shielded |
|
Buccaneer S.2** |
$36,777,979 |
JP8 |
7.26 tons |
28.9 tons |
2 |
19 |
Radar (120 km), FLIR (12 km) |
Shielded |
|
Aircraft |
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
|
|
Buccaneer S.1 |
2644 |
734 (140) |
NA
199 7/4
70/40 |
9240 |
4323 |
13715 |
FF5
CF6 RF5
T4 W4 |
|
Buccaneer S.2 |
3610 |
1002 (140) |
NA
270 7/4
70/40 |
9240 |
3026 |
13715 |
FF5
CF6 RF5
T4 W4 |
|
Buccaneer S.2* |
3590 |
999 (140) |
NA
270 7/4
70/40 |
9240 |
3026 |
13715 |
FF5
CF6 RF5
T4 W4 |
|
Buccaneer S.2** |
3578 |
994 (140) |
NA
268 7/4
70/40 |
9240 |
3026 |
13715 |
FF5
CF6 RF5
T4 W4 |
|
Aircraft |
Combat Equipment |
Minimum Landing/Takeoff
Zone |
RF |
Armament |
Ammo |
|
Buccaneer S.1 |
IFF, Secure Radios, RWR, Stealth 1 |
1800/1600 Hardened Runway |
+3 |
Internal Weapon Bay (1.81 tons), 4
hardpoints |
None |
|
Buccaneer S.2 |
IFF, Secure Radios, RWR, Stealth 1 |
1800/1600 Hardened Runway |
+3 |
Internal Weapon Bay (1.81 tons), 4
hardpoints |
None |
|
Buccaneer S.2* |
IFF, Secure Radios, RWR, ECM 1, Stealth
1, HUD, Flare/Chaff (30/20) |
1800/1600 Hardened Runway |
+3 |
Internal Weapon Bay (1.81 tons), 4
hardpoints |
None |
|
Buccaneer S.2** |
IFF, Secure Radios, RWR, ECM 1, IRCM 1,
Flare/Chaff (30/20), EW Suite, Stealth 1, HUD Interface |
1800/1600 Hardened Runway |
+4 |
Internal Weapon Bay (1.81 tons), 4
hardpoints |
None |
Hawker Hunter
Notes: This jet
is a mid-1960s relic that is still in wide use by Lebanon, though recently they
have been looking at ex-US F-16Cs and Ds to replace them. Its low-power engine
does not lend itself to speed, maneuverability, or lifting power, and its lack
of an afterburner does not give it good acceleration.
However, it is a decent ground attack aircraft, and its four 30mm
autocannons pack quite a punch. The
Hunter formed part of the air forces of 21 nations at one time, though as stated
only Lebanon still flew them as late as 2014. Two seat advanced trainers
remained in RAF service until the 1990s. The Hunter has seen combat service in
conflicts ranging from the Suez Crisis of 1956 to assorted tangles in the
Mideast as late as the 1990s. The Hunter has an ejection seat, but is not
capable of inflight refueling.
Though the
aircraft has a lot of hardpoints, eight of these may only be used for rocket
pods or single rockets, with a load limit of 100 kg per hardpoint; if these
hardpoints are used, the two center wing hardpoints may not be used.
If the two center hardpoints are used, the eight rocket hardpoints may
not be used. The other two fuselage and two wing hardpoints may be used
normally. The Hunter has the rare ability to fire only half its cannons at a
time, if desired, usually done to save ammunition when attacking soft targets or
to load different guns with different types of ammunition. The initial P.1067
prototype was powered by a Rolls Royce Avon 103 turbojet developing 6500 pounds
thrust; the second prototype was powered by an Avon 107 developing 7550 pounds
thrust, and the third prototype was powered by an Armstrong Siddeley Sapphire
101 developing 8000 pounds of thrust. The first two engines tended to flameout
if gun exhaust got into the air intakes in some situations; the Sapphire engine
does not have this problem, but the Sapphire tended to wear fast and needed a
lot of work to forestall engine failures in flight. Production F.1s use the Avon
107 engine, along with the F.4, while the F.2 and F.5 use the Sapphire engine.
F.4s and F.5s had more and larger fuel tanks, including four flexible bag-type
tanks for the wings. The F.4s and F.5s also have diverted gun exhaust to solve
the engine flameout problems, and features a collection mechanism and space for
the cannon armament links instead of the links being ejected overboard and
striking the aircraft’s underside. (The links were collected to blisters under
the cockpit, leading for the aircraft to be called “Sabrinas” by the crews,
after a contemporary movie star.) F.1s and F.2s suffered from short legs, able
to remain in flight for less than an hour, severely restricting their use.
F4s and F5s have much larger fuel tankage but are still restricted in
flight duration.
The F.6 was
powered by an Avon 207 turbojet with an axial compressor, wringing more thrust
out a small engine, to produce 10,145 pounds thrust. The F.6 could haul more
ordnance and fly faster and climb faster, and some late versions were modified
to carry AIM-9 Sidewinder air-to-air missiles on the outboard wing hardpoints.
The F.6 has leading edge dog-tooth extensions halfway down the wing, giving the
aircraft better low-speed flight characteristics. When the BAe Lightning took
over the interceptor role from the F.6, the F.6 was modified into the FGA.9
dedicated ground support aircraft, with a gunsight designed for ground attack
and the addition of an IFF to help prevent fratricide, and avionics to increase
pilot stick authority during ground attack maneuvers. The wings are also
strengthened.
The T.7 and T.8
are the trainer versions of the F.4 and F.5, respectively. These versions are
heavier than their base aircraft, and the pilot and student sit side by side in
a widened fuselage. The T.8 was used primarily as Blackburn Buccaneer conversion
trainers, and were often equipped with pared-down versions of Buccaneer systems;
the T.8B has the cannons and gun ranging-radar removed and replaced with TACAN
and IFIS as well as a lesser variant of the Buccaneer’s avionics suite. The T.8
and T.8B are equipped with arresting hooks.
Twilight 2000
Notes: The Hunter’s primary playground during the Twilight War was the Middle
East; they were taken out of storage by several Middle Eastern countries during
that war to replace aircraft losses.
Merc 2000:
Another non-descript aircraft used by mercs.
|
Aircraft |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
Hunter F.1 |
$6,014,811 |
JP8 |
2.54 tons |
11.16 tons |
1 |
17 |
None |
Enclosed |
|
Hunter F.2 |
$6,066,264 |
JP8 |
2.54 tons |
11.31 tons |
1 |
17 |
None |
Enclosed |
|
Hunter F.4 |
$6,015,611 |
JP8 |
2.54 tons |
11.61 tons |
1 |
17 |
None |
Enclosed |
|
Hunter F.5 |
$6,067,064 |
JP8 |
2.54 tons |
11.81 tons |
1 |
17 |
None |
Enclosed |
|
Hunter F.6 |
$6,591,053 |
JP8 |
3.4 tons |
12.18 tons |
1 |
17 |
None |
Enclosed |
|
Hunter FGA.9 |
$6,594,827 |
JP8 |
3.4 tons |
12.18 tons |
1 |
17 |
None |
Enclosed |
|
Hunter T.7 |
$6,015,154 |
JP8 |
2.54 tons |
12.01 tons |
2 |
17 |
None |
Enclosed |
|
Hunter T.8 |
$6,066,607 |
JP8 |
2.54 tons |
12.16 tons |
2 |
17 |
None |
Enclosed |
|
Hunter T.8B |
$5,236,821 |
JP8 |
2.54 tons |
12.35 tons |
2 |
18 |
Radar (40 km) |
Enclosed |
|
Aircraft |
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
|
|
Hunter F.1 |
3520 |
978 (140) |
NA
264 7/4
70/40 |
1200 |
2299 |
15000 |
FF5
CF4 RF4
T4 W4 |
|
Hunter F.2 |
3676 |
1020 (140) |
NA
276 7/4
70/40 |
1200 |
2434 |
15000 |
FF5
CF4 RF4
T4 W4 |
|
Hunter F.4 |
3386 |
940 (140) |
NA
254 7/4
70/40 |
1800 |
2299 |
15000 |
FF5
CF4 RF4
T4 W4 |
|
Hunter F.5 |
3522 |
978 (140) |
NA
264 7/4
70/40 |
1800 |
2434 |
15000 |
FF5
CF4 RF4
T4 W4 |
|
Hunter F.6 |
3924 |
1200 (135) |
NA
324 7/4
70/40 |
1740 |
3091 |
15000 |
FF5
CF4 RF4
T4 W4 |
|
Hunter FGA.9 |
3924 |
1200 (120) |
NA
324 7/4
70/40 |
1740 |
3091 |
15000 |
FF5
CF4 RF4
T4 W4 |
|
Hunter T.7 |
3276 |
910 (140) |
NA
246 7/4
70/40 |
1800 |
2299 |
15000 |
FF5
CF4 RF4
T4 W4 |
|
Hunter T.8 |
3422 |
950 (140) |
NA
256 7/4
70/40 |
1800 |
2434 |
15000 |
FF5
CF4 RF4
T4 W4 |
|
Hunter T.8B |
3370 |
936 (140) |
NA
252 7/4
70/40 |
1800 |
2434 |
15000 |
FF5
CF4 RF4
T4 W4 |
|
Aircraft |
Combat Equipment |
Minimum Landing/Takeoff
Zone |
RF |
Armament |
Ammo |
|
Hunter F.1 |
None |
1200/800m Hardened Runway |
+2 |
4x30mm Aden Autocannons, 14 Hardpoints* |
600x30mm |
|
Hunter F.2 |
None |
1200/800m Hardened Runway |
+2 |
4x30mm Aden Autocannons, 14 Hardpoints* |
600x30mm |
|
Hunter F.4 |
None |
1200/800m Hardened Runway |
+2 |
4x30mm Aden Autocannons, 14 Hardpoints* |
600x30mm |
|
Hunter F.5 |
None |
1200/800m Hardened Runway |
+2 |
4x30mm Aden Autocannons, 14 Hardpoints* |
600x30mm |
|
Hunter F.6 |
None |
1200/700m Hardened Runway |
+3 |
4x30mm Aden Autocannons, 14 Hardpoints* |
600x30mm |
|
Hunter FGA.9 |
IFF, Secure Radios |
1200/700m Hardened Runway |
+3 |
4x30mm Aden Autocannons, 14 Hardpoints* |
600x30mm |
|
Hunter T.7 |
None |
1200/800m Hardened Runway |
+2 |
4x30mm Aden Autocannons, 14 Hardpoints* |
600x30mm |
|
Hunter T.8 |
None |
1200/800m Hardened Runway |
+2 |
4x30mm Aden Autocannons, 14 Hardpoints* |
600x30mm |
|
Hunter T.8B |
IFF, Secure Radios, RWR |
1200/800m Hardened Runway |
+2 |
14 Hardpoints* |
None |
*See Notes Above
BAC Strikemaster
Notes: This
light strike aircraft was developed from a jet trainer known as the Jet Provost.
It is an unsophisticated aircraft for basic ground support missions, and
is easy to maintain and inexpensive to operate.
The aircraft has ejection seats, but is not capable of in-flight
refueling. The Strikemaster is advertised as a light attack aircraft, but most
customers who bought the Strikemaster actually employed it as an advanced
trainer that could also train aircrews on ground attack missions. The
Strikemaster did see combat service in the air forces of Ecuador, Oman, and
Yemen (though the status of Yemen’s Strikemasters is unknown at this time). The
Strikemaster is or was flown by several African nations as well as Saudi Arabia,
Kuwait, and New Zealand; a total of ten countries flew or still fly the
Strikemaster. Several Strikemasters
were sold off to civilian concerns, and some of these are still flying. The
Strikemaster is still in service in 2025, though sourcing spare parts is getting
difficult since BAC does not make them anymore.
The Strikemaster
is powered by a single uprated Armstrong Siddeley Viper turbojet developing 3140
pounds of thrust. The wings are straight and the fuselage wide, with wider
section for the cockpit. The pilot
and weapons officer sit side by side.
The wings each have two hardpoints; there are no fuselage hardpoints. In
addition, each wingtip carries conformal fuel tanks with a capacity of 284
liters each. In the nose of the Strikemaster are a pair of machineguns; these
are similar to the coaxial armament of some of the world’s tanks and AFVs, being
modified MAG-58 machineguns. (The nose cone houses a G90 gun camera.)
Twilight 2000 Notes: Generally used as a Sandy by NATO air forces, they
were also adapted to operate from carriers, and often found themselves operating
from US carriers. Many of their roles were taken over by Jaguar strike aircraft.
|
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
$1,436,300 |
JP8 |
1.4 tons |
5.22 tons |
2 |
13 |
None |
Enclosed |
|
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
Armor |
|
2850 |
648 (95) |
NA
174 9/6
90/60 |
1660 |
929 |
12200 |
FF4
CF3 RF3
T3 W3 |
|
Combat Equipment |
Minimum Landing/Takeoff
Zone |
RF |
Armament |
Ammo |
|
Secure Radios |
400/500m Primitive Runway |
+1 |
2xMAG, 4 Hardpoints |
1100x7.62mm |