Dassault/Dornier
Alpha Jet
Notes: This is
an aircraft that is a trainer during peacetime and a light strike aircraft
during wartime. It is used by
Belgium, Egypt, France, Ivory Coast, Morocco, Nigeria, Qatar, Togo, Portugal,
Germany, and Cameroon. The
aircraft's two-seat version is used as a trainer or FAC aircraft, but during
wartime strike missions, the back seat is removed and replaced by an electronics
suite that gives it a RWR and ECM emitter.
Of its five hardpoints, only the wings' 4 hardpoints may be used for drop
tanks. The fuselage station is
normally used by a gun pod, as the aircraft has no internal guns, but it may be
used for other stores.
The Alpha Jet’s
airframe is kept intentionally simple; it won’t soak up much damage, but
maintenance is easier than most aircraft of its size and role. The wings and air
intakes are likewise simple and fixed in construction, with conventional flight
surfaces, though power-assisted. Combat variants are designed to have quick
turn-around times, with the Alpha Jet A having a 10-minute turn around when the
ground crew is ready, positioned, and equipped for such. Attack versions can
carry a wide variety of stores, from ECM pods to laser designators to smart
bombs. The avionics of the basic versions is likewise austere, though versions
like the Alpha Jet 2 and Lancier have more modern instrumentation. Most Alpha
Jets are powered by two SNECMA Larzac 04-C5 turbofans each with 2980 pounds
thrust, while the Alpha Jet 2 and Lancier are powered by twin Larzac 04-C20
turbofans each with 3278 pounds thrust.
The Alpha Jet
MS2 is a version designed for Egypt and also sold to Cameroon. It featured a
SAGEM ULISS 81 INS, a Thomson-CSF VE-110 HUD, a TMV630 laser rangefinder in a
modified nose, a TRT AHV 9 radio altimeter, and avionics linked through a
digital computer. The Alpha Jet ACAS adds a laser rangefinder in a modified
nose, as well as INS and a computerized attack system.
The Alpha Jet 2 uses a more powerful engine and is capable of air-to-air
combat with heat-seeking missiles (usually Matra Magics or AIM-9 Sidewinders);
it does not have the laser designator, but otherwise has a blend of the ACAS’s
and MS2’s electronics. (Egyptian Alpha Jets were reportedly upgraded to the
Alpha Jet 2 standard in the late 1980s.)
The Alpha Jet
Lancier (also known as the Alpha Jet 3) adds radar, a multifunction display, a
laser rangefinder, an internal cannon, and integral smart munition delivery
capability, as well as expanding air-to-air combat capability.
The Alpha Jet Lancier sacrifices its belly hardpoint for the cannon
installation. German-built aircraft use the Mauser autocannon, while
French-built Lanciers use the DEFA autocannon.
|
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
Alpha Jet E |
$2,013,780 |
JP5 |
2.5 tons |
7.5 tons |
2 |
15 |
None |
Enclosed |
|
Alpha Jet A |
$4,539,170 |
JP5 |
2.5 tons |
7.55 tons |
1 |
15 |
None |
Enclosed |
|
Alpha Jet MS2 |
$3,637,976 |
JP5 |
2.5 tons |
7.6 tons |
1 |
15 |
None |
Enclosed |
|
Alpha Jet ACAS |
$10,861,856 |
JP5 |
2.5 tons |
7.62 tons |
1 |
12 |
None |
Enclosed |
|
Alpha Jet 2 |
$7,070,460 |
JP5 |
2.55 tons |
8.03 tons |
1 |
12 |
FLIR (12 km) |
Enclosed |
|
Alpha Jet Lancier |
$18,648,274 |
JP5 |
2.55 tons |
9.53 tons |
2 |
16 |
FLIR (30 km), Radar (74 km) |
Enclosed |
|
Vehicle |
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
Armor |
|
Alpha Jet E |
4120 |
1144 (110) |
NA
308 6/3
60/30 |
2160 |
1208 |
13700 |
FF3
CF4 RF3
T2 W3 |
|
Alpha Jet A |
4094 |
1138 (110) |
NA
308 6/3
60/30 |
2160 |
1208 |
13700 |
FF3
CF4 RF3
T2 W3 |
|
Alpha Jet MS2 |
4068 |
1130 (110) |
NA
306 6/3
60/30 |
2160 |
1208 |
13700 |
FF3
CF4 RF3
T2 W3 |
|
Alpha Jet ACAS |
4056 |
1126 (110) |
NA
304 6/3
60/30 |
2160 |
1208 |
13700 |
FF3
CF4 RF3
T2 W3 |
|
Alpha Jet 2 |
4234 |
1176 (110) |
NA
318 6/3
60/30 |
2160 |
1330 |
13700 |
FF3
CF4 RF3
T2 W3 |
|
Alpha Jet Lancier |
3576 |
994 (110) |
NA
268 6/3
60/30 |
2160 |
1330 |
13700 |
FF3
CF4 RF3
T2 W3 |
|
Vehicle |
Combat Equipment |
Minimum Landing/Takeoff
Zone |
RF |
Armament |
Ammo |
|
Alpha Jet E |
None |
550/495m Hardened Runway |
+2 |
5 Hardpoints |
None |
|
Alpha Jet A |
RWR, ECM 2 |
550/495m Hardened Runway |
+2 |
5 Hardpoints |
None |
|
Alpha Jet MS2 |
RWR, INS, HUD, Laser Rangefinder |
550/495m Hardened Runway |
+4 |
5 Hardpoints |
None |
|
Alpha Jet ACAS |
RWR, ECM 2, INS, Laser Designator (6 km) |
550/495m Hardened Runway |
+3 |
5 Hardpoints |
None |
|
Alpha Jet 2 |
RWR, ECM 2, INS, HUD |
550/495m Hardened Runway |
+3 |
5 Hardpoints |
None |
|
Alpha Jet Lancier |
RWR, ECM 3, INS, HUD, Flare/Chaff
(34/25), IR Uncage, Laser Designator (12 km) |
550/495m Hardened Runway |
+4 |
27mm Mauser BK-27 or 30mm DEFA 552, 4
Hardpoints |
300x27mm or 30mm |
AMX International
A-1/A-11 Ghibli
Notes: This is a
joint project of Italy and Brazil, but initiated by the Italians, who wanted a
replacement for their outdated Aeritalia G.91 attack aircraft.
The Brazilians signaled their interest in the program, as they wanted to
replace almost equally outdated Aermacchi MB326s, and they had worked with the
Italians successfully before. Aermacchi, Aeritalia and Brazilian aircraft
manufacturer Embraer set up a consortium, calling it AMX International. The
Brazilians designated their version the A-1; the Italians called theirs the A-11
Ghibli (the Italian word for a scirocco). The Italian and Brazilian models are
similar avionics-wise, but the autocannons equipping the two versions are very
different.
The aircraft has
a day-night capability and is very stable at low speeds as well as high speeds.
Brazilian aircraft have two 30mm cannons, while Italian versions have a
20mm Vulcan; the US at the time denied the sale of Vulcans to Brazil.
The two wingtip hardpoints may only be used for air-to-air missiles or EW
pods; the four underwing hardpoints are “wet,” able to use drop tanks. The A-1
is also set up to carry a pallet-mounted reconnaissance suite on the centerline
hardpoint. The radar mounted is different for each customer. The A-11 is fitted
for air-to-air refueling, while the A-1 is not. Both aircraft are powered by a
Rolls-Royce Spey 807 turbofan, with 11,000 pounds thrust; the US again denied
the sale of the original choice of GE turbofans. In addition, the A-11 has some
extra low-speed handling control surfaces and can takeoff, land, and handle
low-speed flight easier. A-11s were upgraded in 2005 with INS modules, a new
cockpit display, and software enabling the A-11 to drop JDAM-equipped bombs.
This version is designated the A-11A. A-1s were upgraded in 2007 with new
cockpits, updated avionics, and the ability to carry a wider array of weapons.
This is designated the A-1A. In both cases, new, miniaturized avionics lightens
the aircraft slightly.
A-1s and A-11s
normally operate in pairs, one carrying a laser designator on a hardpoint and
spotting for the other. Italian A-11s saw combat service in Bosnia and in Kosovo
(noted for their use of Mk 82 500-pound bombs fitted with Israeli laser-guided
bomb Opher kits). Italian A-11s replaced Tornadoes in the reconnaissance role in
Afghanistan. In 2011, A-11s were again in combat, in the Libyan Intervention.
Italian A-11s were retired from Italian service in 2024. Brazilian A-1s have
seen combat service in a number of counterinsurgency roles, and the latest
upgrade will see them in service until at least 2027.
|
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
A-1 |
$11,361,790 |
JP5 |
3.8 tons |
13 tons |
1 |
16 |
Radar (40 km) |
Shielded |
|
A-1A |
$10,026,190 |
JP5 |
3.8 tons |
12.95 tons |
1 |
16 |
Radar (40 km) |
Shielded |
|
A-11 |
$12,274,832 |
JP5 |
3.8 tons |
13.17 tons |
1 |
17 |
Radar (50 km) |
Shielded |
|
A-11A |
$10,826,402 |
JP5 |
3.8 tons |
13.12 tons |
1 |
17 |
Radar (50 km) |
Shielded |
|
Vehicle |
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
Armor |
|
A-1 |
4378 |
1216 (120) |
NA
328 8/4
50/25 |
3555 |
2226 |
13000 |
FF3
CF3 RF3
T2 W3 |
|
A-1A |
4394 |
1220 (120) |
NA
330 8/4
50/25 |
3555 |
2226 |
13000 |
FF3
CF3 RF3
T2 W3 |
|
A-11 |
4322 |
1200 (110) |
NA
324 8/4
50/25 |
3555 |
2226 |
13000 |
FF3
CF3 RF3
T2 W3 |
|
A-11A |
4338 |
1204 (110) |
NA
326 8/4
50/25 |
3555 |
2226 |
13000 |
FF3
CF3 RF3
T2 W3 |
|
Vehicle |
Combat Equipment |
Minimum Landing/Takeoff
Zone |
RF |
Armament |
Ammo |
|
A-1 |
RWR, Flare/Chaff (30/20), ECM 2, Secure
Radios, All-Weather Flight |
1178/982m Hardened Runway |
+2 |
2x30mm DEFA 554, 7 Hardpoints |
400x30mm |
|
A-1A |
RWR, Flare/Chaff (30/20), ECM 2, Secure
Radios, All-Weather Flight |
1178/982m Hardened Runway |
+3 |
2x30mm DEFA 554, 7 Hardpoints |
400x30mm |
|
A-11 |
RWR, Flare/Chaff (35/35), ECM 2, IRCM 1,
Secure Radios, All-Weather Flight |
600/500m Hardened Runway |
+2 |
20mm M61A1 Vulcan, 7 Hardpoints |
400x20mm |
|
A-11A |
IFF, INS, RWR, Flare/Chaff (35/35), ECM
2, IRCM 1, Secure Radios, All-Weather Flight, |
600/500m Hardened Runway |
+3 |
20mm M61A1 Vulcan, 7 Hardpoints |
400x20mm |
McDonnell Douglas
AV-8B Harrier II
Notes: The
Harrier is a VSTOL multirole aircraft able to perform as both a fighter and
attack aircraft. It is used by
Britain, the US Marines, Italy, India, and Spain.
It has a raised cockpit for superior visibility, a composite material
wing for lightness and strength, and a redesigned nose with air-to-air/ground
radar. It is based on the first
generation of the Harrier strikefighter, pioneered by Britain, hence the Harrier
II. It was designed from the start to be an improved Harrier; efforts
centered around a larger and more powerful version of the Rolls-Royce Pegasus
engine which powered the original Harrier.
Consequently, the Harrier II is a larger version of the Harrier, with
larger wings and more hardpoints. Later upgrades added night vision, producing
the AV-8B(NA) (for Night Attack) and the AV-8B Harrier II Plus. Harrier IIs have
seen action in Gulf War, Iraq War, Afghanistan War, and in Libya in 2011.
Italian and Spanish Harriers have likewise seen combat service as part of NATO
coalitions in those wars and in the former Yugoslavia. Harrier Iis have suffered
from a high accident rate, and the Harrier II is a rather unforgiving aircraft
to fly, particularly in the transition phase from vertical to forward flight and
vice versa. USMC Harrier Iis are almost totally replaced by the F-35B (one
assault carrier must still have its deck reinforced for the F-35B’s hotter
exhaust; as of November 2025; final US Harrier retirement is scheduled for the
second half of 2027), and Italian AV-8Bs are also being replaced by the F-35B.
Spain is considering the move to F-35Bs. Spain designated their Harriers
the EAV-8B, with the trainer versions designated TAV-8B. Royal Navy variants are
designated the Harrier GR.7.
The Harrier II
has a larger wing, and is equipped with leading edge root extensions (LERX) for
improved low-speed handling. The aircraft has an ejection seat and is capable of
in-flight refueling. When
performing VIFF flight, the Harrier has an especially high heat signature, and
attacks with heat-seeking missiles are one level easier.
VTO flight may only be performed by removing 2.4 tons from the cargo
capacity or fuel of the stock AV-8B or 1.1 tons from later models. The Harrier
II is powered by an F402-RR-404A engine with a power of 21,450 pounds of thrust.
The Harrier II features a supercritical wing for increased high-speed (subsonic)
handling and a HOTAS stick and throttle layout. To further increase handling at
both low and high speeds, the taller vertical stabilizer of the Sea Harrier is
used instead of the shorter stabilizer of the AV-8A (the USMC designation of the
original Harrier). The Harrier uses an early Direct Voice Input version, later
used in other aircraft.
Variants include
the TAV-8B trainer (not elaborated here), the AV-8B(NA) version with a
long-range FLIR and more powerful Pegasus 11 engine (23500 pounds thrust), and
the AV-8B Harrier II Plus with improvements on the AV-8B(NA) like increased
chaff and flare capacities and inertial navigation and a radar. The AV-8B(NA)
and plus normally sacrifice one of their wing hardpoints to carry a Litening
targeting pod.
For a short time
in the late 1990s, the US considered an upgrade into a Harrier III variant. This
version would have a helmet-mounted cueing system, an upgraded Pegasus engine
that produced 4000 pounds more thrust (25,450 pounds thrust total), a larger
wing with an extra hardpoint on each one and carrying more fuel (and due to
their increased wingspan, the wingtips would fold), the use of the F-16’s APG-66
radar, and the ability to use weapons like the AIM-132 ASRAAM and AIM-120
AMRAAM, advanced defensive measures such as ECM, ECCM, and IRCM, and Link 16
communications and data-sharing measures. A “what-if” version is presented
below.
|
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
AV-8B Harrier II |
$11,393,694 |
JP4, JP8 |
6 tons |
14.1 tons |
1 |
25 |
None |
Enclosed |
|
Harrier GR.7 |
$11,987,080 |
JP4, JP8 |
6 tons |
14 tons |
1 |
25 |
None |
Enclosed |
|
AV-8B(NA) Harrier II |
$16,050,780 |
JP4, JP8 |
6 tons |
14.45 tons |
1 |
26 |
FLIR (30 km) |
Enclosed |
|
AV-8B Harrier II Plus |
$16,516,530 |
JP4, JP8 |
6 tons |
14.69 tons |
1 |
27 |
Radar (70 km), FLIR (30 km) |
Enclosed |
|
AV-8C Harrier III |
$24,911,611 |
JP4, JP8 |
7 tons |
15.9 tons |
1 |
27 |
Radar (150 km), FLIR (35 km) |
Enclosed |
|
Vehicle |
Tr Mov |
Com Mov* |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
Armor |
|
AV-8B Harrier II |
7850 |
2180 (110) |
NA
588 9/5
60/40 |
4200 |
4358 |
15200 |
FF6
CF6 RF6
W5 T5 |
|
Harrier GR.7 |
7906 |
2196 (110) |
NA
592 9/5
60/40 |
4200 |
4358 |
15200 |
FF6
CF6 RF6
W5 T5 |
|
AV-8B(NA) Harrier II |
8390 |
2330 (110) |
NA
630 9/5
60/40 |
4200 |
4776 |
15240 |
FF6
CF6 RF6
W5 T5 |
|
AV-8B Harrier II Plus |
8254 |
2292 (110) |
NA
618 9/5
60/40 |
4200 |
4776 |
15240 |
FF6
CF6 RF6
W5 T5 |
|
AV-8C Harrier III |
8258 |
2294 (100) |
NA
620 9/5
60/40 |
4620 |
5172 |
|
FF6
CF6 RF6
W6 T5 |
|
Vehicle |
Combat Equipment |
Minimum Landing/Takeoff
Zone |
RF |
Armament |
Ammo |
|
AV-8B Harrier II |
All-Weather Flight, Flare/Chaff (40/25),
RWR |
450/16m (VSTOL) or 450/505m
(Conventional) Primitive Runway |
+2 |
25mm GAU-12/A, 7 Hardpoints |
300x25mm |
|
Harrier GR.7 |
All-Weather Flight, Flare/Chaff (40/25),
RWR |
450/16m (VSTOL) or 450/505m
(Conventional) Primitive Runway |
+2 |
2x25mm ADEN, 7 Hardpoints |
200x25mm |
|
AV-8B(NA) Harrier II |
All-Weather Flight, Flare/Chaff (40/25),
HUD, RWR |
450/16m (VSTOL) or 450/505m
(Conventional) Primitive Runway |
+3 |
25mm GAU-12/A, 7 Hardpoints |
300x25mm |
|
AV-8B Harrier II Plus |
All-Weather Flight, Flare/Chaff (50/30),
HUD, RWR, INS |
450/16m (VSTOL) or 450/505m
(Conventional) Primitive Runway |
+3 |
25mm GAU-12/A, 7 Hardpoints |
300x25mm |
|
AV-8C Harrier III |
All-Weather Flight, Secure Radios, IFF,
Flare/Chaff (55/40), ECM 2, ECCM 1, IRCM 1, HUD, Helmet/Sight Interface,
RWR, INS |
450/16m (VSTOL) or 450/505m
(Conventional) Primitive Runway |
+4 |
25mm GAU-12/A; 9 hardpoints |
300x25mm |
*The Harrier is capable of
reducing its Com Mov to 0, but this is foolhardy in air combat maneuvers.
YuRom IAR-93
Vultur/J-22 Orao
Notes: This is a
strike aircraft jointly produced by Romania and Yugoslavia.
The Soko factory in then-Yugoslavia (now Bosnia) was dismantled in 1992
and never reassembled after that, but the Romanian Avioane Craiova factory
continued to produce Vulturs.
However, in the early 2000s, the Romainians retired the Vultur, and as of July
2019, the Serbian J-22 Oraos were the only examples of this type still flying.
Current status is unknown. This is a light aircraft with a limited weapons load,
but it is cheap and easy to produce.
The Vultur and
Orao are powered by a pair of Rolls-Royce Vipers (produced by license in Bosnia
and designated the Viper Mk 632-41), each outputting 4000 pounds thrust.
This was not the engine the designers wanted; other, more powerful
British engines were preferred, but due to Romania being part of the Warsaw
Pact, Britain would not license any other engine to YuRom. They tried to fit a
domestically designed afterburner to the Viper, but this proved unsuccessful,
and YuRom had to settle for a subsonic aircraft that could only exceed Mach 1 in
a dive. The design is entirely conventional, with swept wings and tail. From
there, the Yugoslavians and Romanians diverged somewhat in design, producing the
Orao and Vultur.
J-22 Orao
The Orao (Eagle)
is designed primarily for close air support and ground attack, with a secondary
mission of low-level interceptor. Two seat variants, designated NJ-22s, were
also produced in small numbers; these were used for tactical reconnaissance
(with the addition of a reconnaissance pod), armed reconnaissance, and as
tactical trainers. The aircraft has gyroscopic navigation, a HUD,
semi-stabilized controls, and two radios, one VHF and one slaved to the
instrument landing system. It is equipped with the Iskra SO-1 RWR and three
chaff/flare dispensers (an individual dispenser could carry flares or chaff
bundles; a typical loadout is presented below).
The Serbian
government undertook a comprehensive upgrade of the Orao’s avionics in the
1990s, designated J-22B Orao 2. This variant incorporated a more powerful engine
with an afterburner, integral wing fuel tanks, higher weight rated hardpoints
(the hardpoints of the Orao were a weak point), and a more advanced Thomson-CSF
HUD. The breakup of Yugoslavia interrupted these upgrades and only 57 were built
before the Yugoslavian Civil War. A two-seat version was planned, but only one
prototype was produced before the Civil War.
After the Civil
War, the Serbians produced a further upgraded J-22, the J-22M1A. This version
adds a Safran Sigma 95 INS, multifunction displays in a glass cockpit, a HUD
interface feature, a compact radar set, and an attack mission computer. These
versions were made using NJ-22s, with the back seat taken out and the space used
for avionics, particularly the mission computer.
IAR-93 Vultur
The IAR-93A
Vultur (Eagle) is mostly the same as the J-22, differing only in detail. The
engines are the same and the avionics are likewise also the same, though perhaps
a little more comprehensive. Relatively more two-seat versions were produced as
a percentage of aircraft, and designated IAR-93ADC. The IAR-93A is a little
lighter than the J-22, and its hardpoints do not have the capacity of the J-22.
The IAR-93B (and its BDC two-seat counterpart), diverge more from its J-22B
cousin; the Romanians did not develop the Vultur as much as did the Serbians
develop the J-22, since after they entered NATO and prior to that from the
Soviet Union, they had access to better aircraft. One thing they did do,
however, was to place cameras all around the aircraft, which the pilot could
access in his MFD. The J-22B’s afterburning, uprated engine is also used on the
IAR-93B, along with an increased fuel load. The Vultur has dog-tooth leading
edge extensions, giving it better low-speed handling.
Twilight 2000
Notes: The Romanian factory manufacturing the Vultur (and some other aircraft)
was put out of action permanently by air strikes in 1999.
|
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
J-22 Orao |
$6,000,747 |
JP8 |
2.8 tons |
11.08 tons |
1 |
15 |
None |
Enclosed |
|
NJ-22 Orao |
$7,090,622 |
JP8 |
2.8 tons |
11.28 tons |
2 |
15 |
None |
Enclosed |
|
J-22B Orao 2 |
$6,352,501 |
JP8 |
3.3 tons |
12.19 tons |
1 |
15 |
None |
Enclosed |
|
J-22M1A Orao 2.0 |
$9,363,405 |
JP8 |
3.3 tons |
12.49 tons |
1 |
17 |
Radar (50 km) |
Enclosed |
|
IAR-93A Vultur |
$6,008,897 |
JP8 |
2.5 tons |
10.9 tons |
1 |
15 |
None |
Enclosed |
|
IAR-93ADC Vultur |
$7,254,247 |
JP8 |
2.5 tons |
11.1 tons |
2 |
15 |
None |
Enclosed |
|
IAR-93B Vultur |
$9,299,476 |
JP8 |
2.5 tons |
12.01 tons |
1 |
15 |
4 CCD Cameras (F, R, RS, LS) |
Enclosed |
|
IAR-93BDC Vultur |
$10,986,360 |
JP8 |
2.5 tons |
12.21 tons |
2 |
15 |
4 CCD Cameras (F, R, RS, LS) |
Enclosed |
|
Vehicle |
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
Jaguar |
|
J-22 Orao |
3750 |
1042 (115) |
NA
242 9/5
90/50 |
3120 |
2434 |
15000 |
FF4
CF4 RF3
T3 W3 |
|
NJ-22 Orao |
3684 |
1024 (115) |
NA
276 9/5
90/50 |
3000 |
2434 |
15000 |
FF4
CF4 RF3
T3 W3 |
|
J-22B Orao 2 |
4256 |
1182 (115) |
NA
320 9/5
90/50 |
3200 |
3045 |
15000 |
FF4
CF4 RF3
T3 W3 |
|
J-22M1A Orao 2.0 |
4156 |
1154 (115) |
NA
312 9/5
90/50 |
3200 |
3045 |
15000 |
FF4
CF4 RF3
T3 W3 |
|
IAR-93A Vultur |
3812 |
1058 (110) |
NA
286 9/5
90/50 |
3120 |
2434 |
15000 |
FF4
CF4 RF3
T3 W3 |
|
IAR-93ADC Vultur |
3744 |
1040 (110) |
NA
280 9/5
90/50 |
3000 |
2434 |
15000 |
FF4
CF4 RF3
T3 W3 |
|
IAR-93B Vultur |
4320 |
1200 (110) |
NA
324 9/5
90/50 |
3300 |
3045 |
15000 |
FF4
CF4 RF3
T3 W3 |
|
IAR-93BDC Vultur |
4250 |
1180 (110) |
NA
318 9/5
90/50 |
3180 |
3045 |
15000 |
FF4
CF4 RF3
T3 W3 |
|
Vehicle |
Combat Equipment |
Minimum Landing/Takeoff
Zone |
RF |
Armament |
Ammo |
|
J-22/NJ-22 Orao |
Flare/Chaff (27/18), HUD, RWR |
950/600m Primitive Runway |
+1 |
2xGSh-23L 23mm Autocannons, 5 Hardpoints |
400x23mm |
|
J-22B Orao 2 |
Flare/Chaff (27/18), HUD, RWR |
950/600m Primitive Runway |
+2 |
2xGSh-23L 23mm Autocannons, 5 Hardpoints |
400x23mm |
|
J-22M1A Orao 2.0 |
Flare/Chaff (27/18), HUD, HUD Interface,
RWR, INS |
950/600m Primitive Runway |
+2 (+3 Air to Ground) |
2xGSh-23L 23mm Autocannons, 5 Hardpoints |
400x23mm |
|
IAR-93A/ADC Vultur |
Secure Radios, Flare/Chaff (27/18), HUD,
RWR, IFF |
940/560m Primitive Runway |
+2 |
2xGSh-23L 23mm Autocannons, 5 Hardpoints |
400x23mm |
|
IAR-93B/BDC Vultur |
Secure Radios, Flare/Chaff (36/27), HUD,
RWR, IFF |
940/560m Primitive Runway |
+3 |
2xGSh-23L 23mm Autocannons, 5 Hardpoints |
400x23mm |
Notes: This is
an attack aircraft produced by an international effort of France and Britain.
It was built by SEPECAT, which is a consortium between Breguet and BAC,
with the engines made by a separate consortium of Rolls-Royce and Turbomeca,
simply called Rolls-Royce Turbomeca. It is also used by Ecuador, India, Nigeria,
and Oman. Two seat versions of this
aircraft exist. This aircraft was a
standout in the 1991 Gulf War, in Indian attacks on Kashmir and Kurdistan, and
in Mauritania, Iraq, Chad, Bosnia and Pakistan. The pilot has an ejection seat,
and the aircraft is capable of inflight refueling. It is also capable of nuclear
weapon delivery. It was replaced in the RAF in 2007 by the Typhoon and in French
service in 2005 by the Rafale; the Indians still fly theirs.
The design of
the Jaguar is orthodox, with a swept wing and tail and twin Adour engines.
The landing gear is long to allow for a variety of large stores to be
carried, most notably a large drop tank on the centerline hardpoint. Two of its
seven hardpoints are unusual; they are on top of the wing, to be used by
air-to-air missiles such as Sidewinders, AIM-132 ASRAAMs, or Matra Magics;
French Jaguars do not have these overwing hardpoints and have only five
hardpoints. Three of its hardpoints
(centerline and the two inner wing hardpoints) may be used for drop tanks in
addition to weapons.
The first
complicated part of the Jaguar partnerships is its Adour turbofans.
In French service, Jaguars were introduced with the base Mk 101 engines,
capable of 5000 pounds thrust each, and equipped with an afterburner. The first
RAF Jaguars were equipped with the Mk 102, which is nearly identical to the Mk
101, but has a higher-efficiency afterburner and greater acceleration, and is
capable of providing 5110 pounds of thrust per engine. The RAF later changed the
engines out for Mk 104s in 1981, which have 5500 pounds thrust, and in 1999 with
the Mk 106, with 6500 pounds thrust. The Mk 804 was an export version powering
Indian Air Force Jaguars and with 7500 pounds thrust; the Mk 811 was another
Indian version developing 8400 pounds thrust. France was constantly jockeying
for the Adours to be built more and more in France, maximizing profit for
Turbomeca, and this caused friction; Rolls-Royce constantly pushed back, causing
more friction.
French Jaguars
have a double gyroscopic navigation system, while RAF Jaguars and Indian Jaguars
have an inertial navigation system. French Jaguars do not have a HUD, while
British and Indian Jaguars do. British GR.1s also have the controversial LRMTS
(Laser Ranging and Marked Targeting System) to help increase bombing and weapons
accuracy; this system is controversial because while the British insisted in its
inclusion in their Jaguars, its reliability is quite low. French aircraft gained
the Atlis II conformal targeting pod starting in the early 1990s; the conformal
pod is low-drag, but does use one of the outer wing hardpoints. GR.1As were
upgraded with the NAVWASS II (NAVigation and Weapon Aiming SubSystem) to allow
accurate navigation and weapon delivery with a radar set being installed.
British GR.1 Jaguars gained a TIALD laser designator in a conformal pod. (These
were designated GR.1B.) The GR.1B was also powered by the more powerful Mk 104
engines. The GR.3 could carry either the TIALD or a camera pod in its conformal
configuration; the GR.3A was also re-engined with the Mk 106 engines. Both have
mild EW protection.
RAF Trainer
versions are also capable of attack missions, but have two seats instead of one,
and are longer and heavier like the Jaguar E. The T2 is based on the GR.1, the
T2A on the GR.1A, the T2B on the GR.1B, and the T4 is based on the GR.3 (but is
actually a T2A upgraded to GR.3-like capabilities). The T2 sacrifices one of its
ADEN autocannons, as the ammunition drum would go where the rear seat and its
avionics go. Another reason to delete the second gun was to counteract the
increase in weight from the second cockpit.
Indian Jaguars
(designated Jaguar IS) were fitted with the Agave radar system, the NAVWASS
navigation and weapon-aiming system (in the case of the first few BAe-built
aircraft), and the DARIN (Display Attack and Ranging Inertial Navigation)
mission computer system (in the case of the subsequent Indian-built Jaguars).
The Indians swapped the TIALD pod for a US-made Litening Pod, which is lighter
in weight. The IAF also equipped their Jaguars with radar, initially the Agave,
then in the early 2000s the radars were changed to the much more capable
EL/M-2052 AESA radar. Late production DARIN III upgrades brought GPS to the
Indian Jaguars and kept the INS set as a backup. The Indians initially used the
Mk 804 engine, upgrading to the Mk 811 engine in the early 2000s. The IM
maritime strike model is the same as the IS, but has no NAVWASS-equipped model,
and is rigged to carry the Sea Eagle antiship missiles. The Jaguar IB is the
two-seat trainer/strike version, similar in concept if not execution to the
British T2.
The Indians were
actually the largest user of the Jaguar and are currently the only Air Force to
be still operating the Jaguar. The Indians do not use the Jaguar in a nuclear
deterrent role, though the Indian Jaguar is capable of nuclear weapon delivery.
Twilight 2000
Notes: The DARIN III-equipped model of the IS does not exist in the Twilight
2000 timeline, nor are any Indian Jaguars fitted with the EM/M-2052 radar.
|
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
Jaguar A (French) |
$13,694,792 |
JP5 |
4.76 tons |
15.7 tons |
1 |
23 |
None |
Shielded |
|
Jaguar A (French w/Atlis II) |
$15,739,592 |
JP5 |
4.48 tons |
15.98 tons |
1 |
24 |
None |
Shielded |
|
Jaguar E (French) |
$14,663,774 |
JP5 |
4.76 tons |
16.14 tons |
2 |
23 |
None |
Shielded |
|
Jaguar E (French w/Atlis II) |
$16,487,774 |
JP5 |
4.48 tons |
16.42 tons |
2 |
24 |
None |
Shielded |
|
Jaguar S (RAF GR.1) |
$13,739,437 |
JP5 |
4.76 tons |
15.08 tons |
1 |
23 |
None |
Shielded |
|
Jaguar S (RAF GR.1A) |
$14,044,027 |
JP5 |
4.76 tons |
15.24 tons |
1 |
23 |
None |
Shielded |
|
Jaguar S (RAF GR.1B) |
$15,863,047 |
JP5 |
4.48 tons |
15.52 tons |
1 |
24 |
None |
Shielded |
|
Jaguar S (RAF GR.3) |
$19,271,047 |
JP5 |
4.48 tons |
15.6 tons |
1 |
25 |
None |
Shielded |
|
Jaguar S (RAF GR.3A) |
$19,560,727 |
JP5 |
4.48 tons |
16.28 tons |
1 |
25 |
None |
Shielded |
|
Jaguar B (RAF T2) |
$12,303,610 |
JP5 |
4.76 tons |
15.12 tons |
2 |
23 |
None |
Shielded |
|
Jaguar B (RAF T2A) |
$12,492,850 |
JP5 |
4.76 tons |
15.28 tons |
2 |
23 |
None |
Shielded |
|
Jaguar B (RAF T2B) |
$14,439,997 |
JP5 |
4.48 tons |
15.56 tons |
2 |
24 |
None |
Shielded |
|
Jaguar B (RAF T4) |
$18,087,970 |
JP5 |
4.48 tons |
15.64 tons |
2 |
25 |
None |
Shielded |
|
Jaguar IS (NAVWASS-Equipped, Agave
Radar) |
$21,656,647 |
JP5 |
4.48 tons |
17.05 tons |
1 |
25 |
Radar (74 km) |
Shielded |
|
Jaguar IS (DARIN-Equipped, Agave Radar,
Mk 804 Engines) |
$20,800,387 |
JP5 |
4.62 tons |
16.91 tons |
1 |
25 |
Radar (74 km) |
Shielded |
|
Jaguar IS (DARIN-Equipped, Agave Radar,
Mk 811 Engines) |
$21,969,247 |
JP5 |
4.62 tons |
17.51 tons |
1 |
25 |
Radar (74 km) |
Shielded |
|
Jaguar IS (DARIN-Equipped, EM/M-2052
Radar, Mk 804 Engines) |
$21,550,147 |
JP5 |
4.62 tons |
17.31 tons |
1 |
25 |
Radar (200 km) |
Shielded |
|
Jaguar IS (DARIN-Equipped, EM/M-2052
Radar, Mk 811 Engines) |
$21,810,007 |
JP5 |
4.62 tons |
17.91 tons |
1 |
25 |
Radar (200 km) |
Shielded |
|
Jaguar IS (DARIN III, EM/M-2052 Radar,
Mk 811 Engines) |
$22,662,007 |
JP5 |
4.62 tons |
17.91 tons |
1 |
26 |
Radar (200 km) |
Shielded |
|
Jaguar IB (NAVWASS-Equipped, Agave
Radar) |
$20,956,210 |
JP5 |
4.48 tons |
17.09 tons |
2 |
25 |
Radar (74 km) |
Shielded |
|
Jaguar IB (DARIN-Equipped, Agave Radar,
Mk 804 Engines) |
$19,725,010 |
JP5 |
4.62 tons |
16.95 tons |
2 |
25 |
Radar (74 km) |
Shielded |
|
Jaguar IB (DARIN-Equipped, Agave Radar,
Mk 811 Engines) |
$20,003,170 |
JP5 |
4.62 tons |
17.55 tons |
2 |
25 |
Radar (74 km) |
Shielded |
|
Jaguar IB (DARIN-Equipped, EM/M-2052
Radar, Mk 804 Engines) |
$20,527,570 |
JP5 |
4.62 tons |
17.35 tons |
2 |
25 |
Radar (200 km) |
Shielded |
|
Jaguar IB (DARIN-Equipped, EM/M-2052
Radar, Mk 811 Engines) |
$20,805,730 |
JP5 |
4.62 tons |
17.95 tons |
2 |
25 |
Radar (200 km) |
Shielded |
|
Vehicle |
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
Jaguar |
|
Jaguar A (French) |
3296 |
916 (120) |
NA
248 8/4
80/40 |
4200 |
2015 |
14000 |
FF4
CF4 RF3
T3 W4 |
|
Jaguar A (French w/Atlis II) |
3262 |
906 (120) |
NA
244 8/4
80/40 |
4200 |
2015 |
14000 |
FF4
CF4 RF3
T3 W4 |
|
Jaguar E (French) |
3230 |
898 (120) |
NA
242 8/4
80/40 |
4200 |
2015 |
14000 |
FF4
CF4 RF3
T3 W4 |
|
Jaguar E (French w/Atlis II) |
3176 |
882 (120) |
NA
238 8/4
80/40 |
4200 |
2015 |
14000 |
FF4
CF4 RF3
T3 W4 |
|
Jaguar S (RAF GR.1) |
3524 |
978 (120) |
NA
272 8/4
80/40 |
4200 |
2072 |
14000 |
FF4
CF4 RF3
T3 W4 |
|
Jaguar S (RAF GR.1A) |
3488 |
968 (120) |
NA
270 8/4
80/40 |
4200 |
2072 |
14000 |
FF4
CF4 RF3
T3 W4 |
|
Jaguar S (RAF GR.1B) |
3688 |
1024 (120) |
NA
286 8/4
80/40 |
4200 |
2234 |
14000 |
FF4
CF4 RF3
T3 W4 |
|
Jaguar S (RAF GR.3) |
3670 |
1020 (120) |
NA
286 8/4
80/40 |
4200 |
2234 |
14000 |
FF4
CF4 RF3
T3 W4 |
|
Jaguar S (RAF GR.3A) |
4150 |
1152 (120) |
NA
322 8/4
80/40 |
4200 |
2642 |
14000 |
FF4
CF4 RF3
T3 W4 |
|
Jaguar B (RAF T2) |
3514 |
976 (120) |
NA
272 8/4
80/40 |
4200 |
2072 |
14000 |
FF4
CF4 RF3
T3 W4 |
|
Jaguar B (RAF T2A) |
3478 |
966 (120) |
NA
270 8/4
80/40 |
4200 |
2072 |
14000 |
FF4
CF4 RF3
T3 W4 |
|
Jaguar B (RAF T2B) |
3680 |
1022 (120) |
NA
286 8/4
80/40 |
4200 |
2234 |
14000 |
FF4
CF4 RF3
T3 W4 |
|
Jaguar B (RAF T4) |
3660 |
1016 (120) |
NA
286 8/4
80/40 |
4200 |
2234 |
14000 |
FF4
CF4 RF3
T3 W4 |
|
Jaguar IS (NAVWASS-Equipped, Agave
Radar) |
4360 |
1266 (120) |
NA
342 8/4
80/40 |
4200 |
3044 |
14000 |
FF4
CF4 RF3
T3 W4 |
|
Jaguar IS (DARIN-Equipped, Agave Radar,
Mk 804 Engines) |
4598 |
1278 (120) |
NA
346 8/4
80/40 |
4200 |
3044 |
14000 |
FF4
CF4 RF3
T3 W4 |
|
Jaguar IS (DARIN-Equipped, Agave Radar,
Mk 811 Engines) |
4968 |
1380 (120) |
NA
372 8/4
80/40 |
4200 |
3410 |
14000 |
FF4
CF4 RF3
T3 W4 |
|
Jaguar IS (DARIN-Equipped, EM/M-2052
Radar, Mk 804 Engines) |
4492 |
1248 (120) |
NA
336 8/4
80/40 |
4200 |
3044 |
14000 |
FF4
CF4 RF3
T3 W4 |
|
Jaguar IS (DARIN-Equipped, EM/M-2052
Radar, Mk 811 Engines) |
4860 |
1350 (120) |
NA
364 8/4
80/40 |
4200 |
3410 |
14000 |
FF4
CF4 RF3
T3 W4 |
|
Jaguar IS (DARIN III, EM/M-2052 Radar,
Mk 811 Engines) |
4860 |
1350 (120) |
NA
364 8/4
80/40 |
4200 |
3410 |
14000 |
FF4
CF4 RF3
T3 W4 |
|
Jaguar IB (NAVWASS-Equipped, Agave
Radar) |
4550 |
1264 (120) |
NA
342 8/4
80/40 |
4200 |
3044 |
14000 |
FF4
CF4 RF3
T3 W4 |
|
Jaguar IB (DARIN-Equipped, Agave Radar,
Mk 804 Engines) |
4586 |
1274 (120) |
NA
344 8/4
80/40 |
4200 |
3044 |
14000 |
FF4
CF4 RF3
T3 W4 |
|
Jaguar IB (DARIN-Equipped, Agave Radar,
Mk 811 Engines) |
4958 |
1378 (120) |
NA
372 8/4
80/40 |
4200 |
3410 |
14000 |
FF4
CF4 RF3
T3 W4 |
|
Jaguar IB (DARIN-Equipped, EM/M-2052
Radar, Mk 804 Engines) |
4482 |
1246 (120) |
NA
336 8/4
80/40 |
4200 |
3044 |
14000 |
FF4
CF4 RF3
T3 W4 |
|
Jaguar IB (DARIN-Equipped, EM/M-2052
Radar, Mk 811 Engines) |
4848 |
1346 (120) |
NA
364 8/4
80/40 |
4200 |
3410 |
14000 |
FF4
CF4 RF3
T3 W4 |
|
Vehicle |
Combat Equipment |
Minimum Landing/Takeoff
Zone |
RF |
Armament |
Ammo |
|
Jaguar A/E (French) |
RWR, Secure Radios, Flare/Chaff (50/40) |
785/580m Hardened Runway |
+1 |
2x30mm DEFA 552 autocannons, 5
hardpoints |
300x30mm |
|
Jaguar A/E (French w/Atlis II) |
RWR, Secure Radios, Flare/Chaff (50/40),
Laser Designator (30 km) |
785/580m Hardened Runway |
+2 |
2x30mm DEFA 552 autocannons, 4
hardpoints |
300x30mm |
|
Jaguar S (RAF GR.1) |
RWR, Secure Radios, Flare/Chaff (50/40),
HUD |
785/580m Hardened Runway |
+2 |
2x30mm ADEN autocannons, 7 hardpoints |
300x30mm |
|
Jaguar S (RAF GR.1A) |
RWR, Secure Radios, Flare/Chaff (50/40),
HUD, IFF |
785/580m Hardened Runway |
+3 |
2x30mm ADEN autocannons, 7 hardpoints |
300x30mm |
|
Jaguar S (RAF GR.1B) |
RWR, Secure Radios, Flare/Chaff (50/40),
HUD, IFF, Laser Designator (30 km) |
785/580m Hardened Runway |
+3 |
2x30mm ADEN autocannons, 6 hardpoints |
300x30mm |
|
Jaguar S (RAF GR.3/3A) |
RWR, Secure Radios, Flare/Chaff (50/40),
HUD, IFF, ECM 1, ECCM 1, Laser Designator (30 km) |
785/580m Hardened Runway |
+3 |
2x30mm ADEN autocannons, 6 hardpoints |
300x30mm |
|
Jaguar B (RAF T2) |
RWR, Secure Radios, Flare/Chaff (50/40),
HUD |
785/580m Hardened Runway |
+2 |
30mm ADEN Autocannon, 7 hardpoints |
150x30mm |
|
Jaguar B (RAF T2A) |
RWR, Secure Radios, Flare/Chaff (50/40),
HUD, IFF |
785/580m Hardened Runway |
+3 |
30mm ADEN Autocannon, 7 hardpoints |
150x30mm |
|
Jaguar B (RAF T2B) |
RWR, Secure Radios, Flare/Chaff (50/40),
HUD, IFF, Laser Designator (30 km) |
785/580m Hardened Runway |
+3 |
30mm ADEN Autocannon, 6 hardpoints |
150x30mm |
|
Jaguar B (RAF T4) |
RWR, Secure Radios, Flare/Chaff (50/40),
HUD, IFF, ECM 1, ECCM 1, Laser Designator (30 km) |
785/580m Hardened Runway |
+3 |
30mm ADEN Autocannon, 6 hardpoints |
150x30mm |
|
Jaguar IS (NAVWASS-Equipped) |
RWR, Secure Radios, Flare/Chaff (50/40),
HUD, IFF, ECM 1, ECCM 1, Laser Designator (30 km) |
785/580m Hardened Runway |
+3 |
2x30mm ADEN autocannons, 6 hardpoints |
300x30mm |
|
Jaguar IS (DARIN-equipped) |
RWR, Secure Radios, Flare/Chaff (50/40),
HUD, IFF, INS, ECM 1, ECCM 1, Laser Designator (30 km) |
785/580m Hardened Runway |
+3 |
2x30mm ADEN autocannons, 6 hardpoints |
300x30mm |
|
Jaguar IS (DARIN III) |
RWR, Secure Radios, Flare/Chaff (50/40),
HUD, IFF, GPS, INS, ECM 1, ECCM 1, Laser Designator (30 km) |
785/580m Hardened Runway |
+4 |
2x30mm ADEN autocannons, 6 hardpoints |
300x30mm |
|
Jaguar IB (NAVWASS-Equipped) |
RWR, Secure Radios, Flare/Chaff (50/40),
HUD, IFF, ECM 1, ECCM 1, Laser Designator (30 km) |
785/580m Hardened Runway |
+3 |
30mm ADEN Autocannon, 6 hardpoints |
150x30mm |
|
Jaguar IB (DARIN-equipped) |
RWR, Secure Radios, Flare/Chaff (50/40),
HUD, IFF, INS, ECM 1, ECCM 1, Laser Designator (30 km) |
785/580m Hardened Runway |
+3 |
30mm ADEN Autocannon, 6 hardpoints |
150x30mm |
Notes: This basic
trainer/light attack aircraft is a joint product of China and Pakistan.
The Chinese name is the Hongdu JL-8, but at the suggestion of the
Pakistani president, the name was changed to reflect its status as an
internationally produced aircraft. Like most aircraft of its class, it is an
unsophisticated aircraft with a light weapon load, being primarily a trainer
with secondary strike capability. Originally, the K-8 was to be produced using a
large amount of components sourced from the US, but embargoes after the
Tiananmen massacre of 1989 caused the developing parties to find their parts
elsewhere. In the end, much of the avionics were approved for the Chinese
variant, and even an American engine was approved for the Pakistani variant.
The K-8 looks
much like the Bae Hawk, being a low-wing aircraft with wings that are straight
at the leading edge. Some of the control surfaces, like the tail surfaces, are
electrically actuated, and some, like the wing surfaces, are hydraulically
actuated. The control surfaces are also hydraulically boosted, with artificial
feel qualities. The cockpit of the K-8 and JL-8 are designed to be as close as
possible to a combat aircraft, while retaining a basically simple layout so as
to not confuse or overload students. The ejection seats are of the zero-zero
type, meaning that safe ejection is possible at zero speed and altitude. Though
the JL-8 and K-8 was designed to have a secondary strike capability, the first
air to ground munitions were only first tested in 2011, even though the first
flight was back in 1993. The K-8/JL-8 have UHF and VHF radios along with a TACAN
receiver and an automatic direction finder. Optionally, an Instrument Landing
System is available, and these are believed to be present in Chinese JL-8s. Air
conditioning and heating are available, even when stationary on the ground. The
JL-8 is powered by a WS-11 turbofan engine developing 3800 pounds thrust.
This engine is a license-produced version of the Ukrainian AL-25TL. The
K-8 is powered by a license-produced Honeywell TFE731 turbofan developing 3600
pounds thrust. Four hardpoints are on the JL-8 and K-8, two under each wing;
there is no centerline hardpoint, except for attachments for a 23mm autocannon
pod. This is reflected below.
The JL-8 is used
by the PLAAF for basic jet training and basic combat training. The K-8 is used
by the Pakistani Air Force for the same thing; the K-8P is the same aircraft
with new avionics, a glass cockpit, and updated ejection seats. The K-8W is an
export variant used by the Venezuelan Bolivarian Air Force and Bangladeshi Air
Force. It has no US-controlled
parts and features an improved cockpit layout and a HUD. The K-8VB is a standard
K-8 used by the Venezuelan Bolivarian Air Force; it is identical to the K-8P for
game purposes. The K-8E is another export model supplied to Egypt, has a cockpit
layout modified to suit Egyptian requirements, and is identical to the JL-8 for
game purposes. The K-8NG (New Generation) is an advanced trainer/strike aircraft
with an air-to-ground precision strike capability, and able to mount laser
designators, smart munitions, and reconnaissance pods. The centerline hardpoint
is added, and able to mount things like laser designators and camera pods; it is
not rated to mount weapons or fuel tanks, except for a 23mm autocannon.
Twilight 2000
Notes: China only began ordering the K-8 just before the Twilight War, and few
were available to Chinese forces. Pakistan built large numbers of them and used
them in conflicts against Indian forces throughout the Twilight War.
|
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
JL-8 |
$3,019,571 |
JP5 |
943 kg |
4.33 tons |
2 |
13 |
None |
Enclosed |
|
K-8 |
$2,973,161 |
JP5 |
943 kg |
4.33 tons |
2 |
13 |
None |
Enclosed |
|
K-8P |
$4,092,461 |
JP5 |
943 kg |
4.33 tons |
2 |
14 |
None |
Enclosed |
|
K-8W |
$4,149,791 |
JP5 |
943 kg |
4.33 tons |
2 |
14 |
None |
Enclosed |
|
K-8NG |
$4,231,691 |
JP5 |
943 kg |
4.33 tons |
2 |
15 |
None |
Enclosed |
|
Vehicle |
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
Armor |
|
JL-8 |
2272 |
632 (100) |
NA
170 6/3
60/30 |
1855 |
770 |
13600 |
FF3
CF3 RF3
T2 W3 |
|
K-8 |
2150 |
598 (100) |
NA
162 6/3
60/30 |
1855 |
728 |
13600 |
FF3
CF3 RF3
T2 W3 |
|
K-8P |
2150 |
598 (100) |
NA
162 6/3
60/30 |
1855 |
728 |
13600 |
FF3
CF3 RF3
T2 W3 |
|
K-8W |
2150 |
598 (100) |
NA
162 6/3
60/30 |
1855 |
728 |
13600 |
FF3
CF3 RF3
T2 W3 |
|
K-8NG |
2150 |
598 (100) |
NA
162 6/3
60/30 |
1855 |
728 |
13600 |
FF3
CF3 RF3
T2 W3 |
|
Vehicle |
Combat Equipment |
Minimum Landing/Takeoff
Zone |
RF |
Armament |
Ammo |
|
JL-8 |
None |
440/400m Hardened Runway |
+1 |
23mm ZU-23 autocannon, 4 hardpoints |
200x23mm |
|
K-8 |
None |
440/400m Hardened Runway |
+1 |
23mm ZU-23 autocannon, 4 hardpoints |
200x23mm |
|
K-8P |
None |
440/400m Hardened Runway |
+1 |
23mm ZU-23 autocannon, 4 hardpoints |
200x23mm |
|
K-8W |
Secure Radios, HUD |
440/400m Hardened Runway |
+2 |
23mm ZU-23 autocannon, 4 hardpoints |
200x23mm |
|
K-8NG |
Secure Radios, HUD |
440/400m Hardened Runway |
+3 |
23mm ZU-23 autocannon, 4 hardpoints |
200x23mm |
Panavia Tornado IDS
Notes: This is
the strike version of the Tornado multirole aircraft (IDS stands for
InterDictor/Strike). It was a joint
venture of Germany, Britain, and Italy, and is or was in service with those
countries and with Saudi Arabia. BAC in Britain and MBB in Germany each had a
42.5% stake in the project, while Aeritalia in Italy had a 15% stake in the
project. A separate composite entity, Turbo-Union, was formed to produce the
RB199 engines for the Tornado, with Rolls-Royce in Britain and MTU in Germany
each having a 40% interest in the engine project, and Fiat of Italy having the
remaining 20%. (Side note, the Tornado was originally called the Panther; I do
not know why they changed the name.)
The Tornado is a
variable geometry aircraft with automatic sweep; the wings change their angle of
sweep in response to changes in airspeed; the automatic sweep angle may be
overridden by the pilot, but the manufacturer does not recommend this.
The wing hardpoints also pivot as the wings’ sweep angle changes. The
crew has ejection seats, and the aircraft is capable of in-flight refueling.
Up to 4 of its hardpoints may be used for drop tanks. The prototypes were
capable of a Mach 1.2 supercruise, but production Tornados with external stores
did not have this ability. Initial Tornado IDSs were powered by two RB199 Mk 101
turbofans, developing 8700 pounds thrust dry and 14840 pounds thrust in
afterburner. The RB199 Mk 103 turbofan engines have a thrust rating of 9105
pounds of thrust each, or 16000 pounds each in afterburner. The Mk 103 powered
the IDS for the longest period of time, including during Desert Storm. These
engines were later replaced with the RB199 Mk 105, with 9555 pounds thrust dry
and 16700 pounds in afterburner. The RB199 is an evolutionary development of the
engines used in the Concorde jetliner. Controls are hydraulic, but actuated by
the fly-by-wire architecture. The fly-by-wire system also makes dozens of
micro-adjustments per second to keep the aircraft stable during its flight and
maneuvers. The Tornado IDS has seven hardpoints, three under the flat fuselage
belly and four under the wings. The Tornado IDS may be configured with up to
four large drop tanks and an underfuselage buddy refueling pod to allow the
Tornado to operate as a tanker. Tornados are able to carry and deploy virtually
any weapon employed by the user country, including in the case of the RAF,
nuclear weapons. The GR.1B is a dedicated antishipping aircraft; it has software
to carry and employ several antishipping weapons, but is otherwise like the GR.1
for game purposes. BAE has tested a Tornado with components made by 3D printing,
and has subsequently been used to replace some parts that required spares,
saving up to 1.2 million Pounds.
Upgrades began
in earnest in the 1990s after experience in Desert Storm. The RAF Tornado IDSs
were made over into GR.4s, with the addition of a FLIR, a wide-angle HUD, and
the software and hardware to carry a slew of new weapons, from Paveway III smart
bombs to Storm Shadow cruise missiles. The software was almost wholly replaced,
with the installation of a new mission computer. The GR.4 can also use the
RAPTOR reconnaissance pod. The GR.4 was further improved into the GR.4A, with
the capability to use the Paveway IV bomb and new radios compatible with the
Link 16 system. In 2000, German IDSs received the ASSTA 1 upgrade, which gave
the ability to use new weapons including the HARM, the Taurus KEPD 350 cruise
missile, the Litening II targeting pod, and Paveway III smart bombs, as well as
the Mk 105 engines. The ASSTA 2 upgrade began in 2005, with new digital avionics
and an EW suite; the ASSTA 3 upgrade in 2008 gave the German Tornados the
ability to pack the JDAM and further upgraded software. The ASSTA 2 and 3
upgrades were applied only to 85 Tornados, since the Tornado is slated to be
replaced by the Eurofighter Typhoon in a short time.
Initial Italian
and Saudi Tornados correspond to the RAF GR.1 and German IDS Mk 1 variants of
the aircraft. The Italians designate their Tornadoes as A-200s. In 2010, the
A-200s received a major upgrade to digital systems and architecture, and the
ability to use a number of new munitions; in game terms, these upgraded A-200s
are otherwise equivalent to the standard A-200 for game purposes. Saudi GR.1s
received upgrades in the 1990s and early 2000s to make them equivalent to the
GR.4A for game purposes, except perhaps for parts scroungers.
|
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
RAF GR.1/German IDS (Mk 101 Engines) |
$66,945,221 |
JP5 |
9 tons |
27.95 tons |
2 |
23 |
Radar (90 km), VAS (30 km) |
Shielded |
|
RAF GR.1/German IDS (Mk 103 Engines) |
$67,497,301 |
JP5 |
9 tons |
28.22 tons |
2 |
23 |
Radar (90 km), VAS (30 km) |
Shielded |
|
RAF GR.4 |
$71,711,237 |
JP5 |
9 tons |
28.58 tons |
2 |
24 |
Radar (90 km), FLIR (60 km), VAS (30 km) |
Shielded |
|
RAF GR.4A |
$72,428,350 |
JP5 |
9 tons |
28.58 tons |
2 |
24 |
Radar (90 km), FLIR (60 km), VAS (30 km) |
Shielded |
|
ASSTA 1 Upgrade |
$67,752,741 |
JP5 |
9 tons |
28.04 tons |
2 |
23 |
Radar (90 km), VAS (30 km) |
Shielded |
|
ASSTA 2 Upgrade |
$71,047,741 |
JP5 |
9 tons |
28.04 tons |
2 |
23 |
Radar (90 km), VAS (30 km) |
Shielded |
|
ASSTA 3 Upgrade |
$71,789,228 |
JP5 |
9 tons |
28.04 tons |
2 |
24 |
Radar (90 km), VAS (30 km) |
Shielded |
|
Vehicle |
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
Armor |
|
RAF GR.1/German IDS (Mk 101 Engines) |
4872 |
1354 (130) |
NA
366 9/6
90/60 |
8000 |
3536 |
19800 |
FF6
CF6 RF6
W5 T5* |
|
RAF GR.1/German IDS (Mk 103 Engines) |
5046 |
1402 (130) |
NA
378 9/6
90/60 |
8000 |
3698 |
19800 |
FF6
CF6 RF6
W5 T5* |
|
RAF GR.4/4A |
5230 |
1452 (130) |
NA
394 9/6
90/60 |
8000 |
3884 |
19800 |
FF6
CF6 RF6
W5 T5* |
|
ASSTA 1/2/3 Upgrade |
5328 |
1480 (130) |
NA
400 9/6
90/60 |
8000 |
3884 |
19800 |
FF6
CF6 RF6
W5 T5* |
|
Vehicle |
Combat Equipment |
Minimum Landing/Takeoff
Zone |
RF |
Armament |
Ammo |
|
RAF GR.1/German IDS |
Flare/Chaff (75/50), RWR, Deception
Jamming (200 km), HUD, IR Uncage, TFR (30 km), Look-Down Radar, Track
While Scan, Laser Designator (60 km), ECM 3, ECCM 2, IRCM 2 |
760/500m Hardened Runway |
+4 |
27mm Mauser BK-27 autocannon, 7
hardpoints |
180x27mm |
|
RAF GR.4/4A |
Flare/Chaff (75/50), RWR, GPS, Deception
Jamming (200 km), HUD, HUD Interface, IR Uncage, TFR (30 km), Look-Down
Radar, Track While Scan, Laser Designator (60 km), ECM 3, ECCM 2, IRCM
2, EW Suite |
760/500m Hardened Runway |
+4 |
27mm Mauser BK-27 autocannon, 7
hardpoints |
180x27mm |
|
ASSTA 1 Upgrade |
Flare/Chaff (75/50), RWR, Deception
Jamming (200 km), HUD, IR Uncage, TFR (30 km), Look-Down Radar, Track
While Scan, Laser Designator (60 km), ECM 3, ECCM 2, IRCM 2 |
760/500m Hardened Runway |
+4 |
27mm Mauser BK-27 autocannon, 7
hardpoints |
180x27mm |
|
ASSTA 2/3 Upgrade |
Flare/Chaff (75/50), RWR, GPS, Deception
Jamming (200 km), HUD, IR Uncage, TFR (30 km), Look-Down Radar, Track
While Scan, Laser Designator (60 km), ECM 3, ECCM 2, IRCM 2, EW Suite |
760/500m Hardened Runway |
+4 |
27mm Mauser BK-27 autocannon, 7
hardpoints |
180x27mm |
*The cockpit has a Kevlar
antispalling liner and has an AV of 7.