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#Post#: 1891--------------------------------------------------
Re: Gondor Factbook
By: Heavenly Paradise Date: June 11, 2015, 9:19 pm
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X-51 Hypersonic Cruise Missile
Speed: Mach 6+
Range: ?
Engine: Scramjet
HTML http://upload.wikimedia.org/wikipedia/commons/4/4b/X-51A_Waverider.jpg
#Post#: 1892--------------------------------------------------
Re: Gondor Factbook
By: Heavenly Paradise Date: June 11, 2015, 9:27 pm
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Self Propelled Artillery
Speed: 37 mph
Crew:2
Range: 311 miles
Armaments: 2x 155mm main guns in over-under barrel arrangement,
1x7.62mm coaxial machine gun, 1x14.7mm antiaircraft machine gun
NBC Protection, Has Night Vision
Powerplant: 1x diesel engine developing 850 horsepower
HTML http://www.militaryfactory.com/armor/imgs/2S35-koalitsiya-sv-coalition-self-propelled-gun-vehicle.jpg
#Post#: 1893--------------------------------------------------
Re: Gondor Factbook
By: Heavenly Paradise Date: June 11, 2015, 9:31 pm
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Anti-radiation Missile
Weight
Length
Diameter
Warhead
section, and later WDU-37/B blast-fragmentation warhead.
Warhead weight
Detonation
mechanism
FMU-111/B laser proximity fuze
Engine
Wingspan
Propellant
Operational
range
150 kilometres; 92 miles (80 nmi)[3]
Speed
Guidance
system
Passive radar homing with home-on-jam, GPS/INS and millimeter
wave active radar homing in E variant.[4] 500-20,000 MHz for
AGM-88C
HTML http://previewcf.turbosquid.com/Preview/2014/05/27__01_10_05/preview1_harm.jpgd444cff2-fd6b-4f27-9b99-82cf7df984b4Larger.jpg
#Post#: 2124--------------------------------------------------
Re: Gondor Factbook
By: Heavenly Paradise Date: June 16, 2015, 6:12 pm
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G-1 Bomber
Crew: four (aircraft commander, copilot, offensive systems
officer and defensive systems officer)
Payload: 125,000 lb (56,700 kg) ; internal and external ordnance
combined
Length: 146 ft (44.5 m)
Wingspan:
Extended: 137 ft (42 m)
Swept: 79 ft (24 m)
Height: 34 ft (10.4 m)
Wing area: 1,950 ft² (181.2 m²)
Airfoil: NACA69-190-2
Empty weight: 192,000 lb (87,100 kg)
Loaded weight: 326,000 lb (148,000 kg)
Max. takeoff weight: 477,000 lb (216,400 kg)
Powerplant: 4 × General Electric F101-GE-102 augmented turbofans
Dry thrust: 14,600 lbf (64.9 kN) each
Thrust with afterburner: 30,780 lbf (136.92 kN) each
Fuel capacity, optional: 10,000 U.S. gal (38,000 L) fuel tank in
1–3 internal weapons bays each
Performance
Maximum speed:
At altitude: Mach 1.25 (721 kn or 830 mph or 1,335 km/h) at
50,000 ft or 15,000 m altitude
At low level: Mach 0.92 (700 mph or 1,100 km/h) at 200–500 ft or
61–152 m altitude
Range: 6,478 nmi (7,455 mi; 11,997 km)
Combat radius: 2,993 nmi (3,444 mi; 5,543 km)
Service ceiling: 60,000 ft (18,000 m)
Wing loading: 167 lb/ft² (816 kg/m²)
Thrust/weight: 0.38
Armament
Hardpoints: six external hardpoints for 50,000 pounds (23,000
kg) of ordnance (use for weapons restricted by arms
treaties[103]) and three internal bomb bays for 75,000 pounds
(34,000 kg) of ordnance.
Bombs:
84× Mk-82 Air inflatable retarder (AIR) general purpose (GP)
bombs[175]
81× Mk-82 low drag general purpose (LDGP) bombs[176]
84× Mk-62 Quickstrike sea mines[177]
24× Mk-84 general purpose bombs
24× Mk-65 naval mines[178]
30× CBU-87/89/CBU-97 Cluster Bomb Units (CBU)[N 2]
30× CBU-103/104/105 Wind Corrected Munitions Dispenser (WCMD)
CBUs
24× GBU-31 JDAM GPS guided bombs (Mk-84 GP or BLU-109 warhead)[N
3]
15× GBU-38 JDAM GPS guided bombs (Mk-82 GP warhead)[N 4]
48x GBU-38 JDAM (using rotary launcher mounted multiple ejector
racks)[179]
48x GBU-54 LaserJDAM (using rotary launcher mounted multiple
ejector racks)[179]
24× AGM-154 Joint Standoff Weapon (JSOW)
96× or 144× GBU-39 Small Diameter Bomb GPS guided bombs[N 5]
(not fielded on B-1 yet)
24× AGM-158 Joint Air to Surface Standoff Missile (JASSM)
24× B61 or B83 nuclear bombs (no longer carried)[178]
Avionics
1× AN/APQ-164 forward-looking offensive Passive electronically
scanned array radar
1× AN/ALQ-161 radar warning receiver and defensive jamming
equipment
1× AN/ASQ-184 defensive management system
1× Sniper Advanced Targeting Pod (optional)[180][181]
[img]
HTML http://www.the-blueprints.com/blueprints-depot/modernplanes/modern-qr/b1b-lancer.GIF[/img]
G-2 Bomber
Crew: 2: pilot and commander (co-pilot)
Length: 69 ft (21.0 m)
Wingspan: 172 ft (52.4 m)
Height: 17 ft (5.18 m)
Wing area: 5,140 ft² (478 m²)
Empty weight: 158,000 lb (71,700 kg)
Loaded weight: 336,500 lb (152,200 kg)
Max. takeoff weight: 376,000 lb (170,600 kg)
Powerplant: 4 × General Electric F118-GE-100 non-afterburning
turbofans, 17,300 lbf (77 kN) each
Fuel Capacity: 167,000 pounds (75,750 kg)
Performance
Maximum speed: Mach 0.95 (550 knots, 630 mph, 1,010 km/h) at
40,000 ft altitude / Mach 0.95 at sea level[150]
Cruise speed: Mach 0.85[65] (487 knots, 560 mph, 900 km/h) at
40,000 ft altitude
Range: 6,000 nmi (11,100 km (6,900 mi))
Service ceiling: 50,000 ft (15,200 m)
Wing loading: 67.3 lb/ft² (329 kg/m²)
Thrust/weight: 0.205
Armament
2 internal bays for ordnance and payload with an official limit
of 40,000 lb (18,000 kg); maximum estimated limit is 50,000 lb
(23,000 kg).[65]
80× 500 lb class bombs (Mk-82, GBU-38) mounted on Bomb Rack
Assembly (BRA)
36× 750 lb CBU class bombs on BRA
16× 2,000 lb class bombs (Mk-84, GBU-31) mounted on Rotary
Launcher Assembly (RLA)
16× B61 or B83 nuclear bombs on RLA (strategic mission)
HTML https://engineeringrussia.files.wordpress.com/2013/04/bomber-970.jpg
G-52 Bomber
General characteristics
Crew: 5 (pilot, copilot, Weapon Systems Officer, navigator,
Electronic Warfare Officer, and tail gunner until the removal of
the tail gun in 1991)
Length: 159 ft 4 in (48.5 m)
Wingspan: 185 ft 0 in (56.4 m)
Height: 40 ft 8 in (12.4 m)
Wing area: 4,000 sq ft (370 m²)
Airfoil: NACA 63A219.3 mod root, NACA 65A209.5 tip
Empty weight: 185,000 lb (83,250 kg)
Loaded weight: 265,000 lb (120,000 kg)
Max. takeoff weight: 488,000 lb (220,000 kg)
Powerplant: 8 × Pratt & Whitney TF33-P-3/103 turbofans, 17,000
lbf (76 kN) each
Fuel capacity: 47,975 U.S. gal (39,948 imp gal; 181,610 L)
Zero-lift drag coefficient: 0.0119 (estimated)
Drag area: 47.60 sq ft (4.42 m²)
Aspect ratio: 8.56
Performance
Maximum speed: 560 kn (650 mph, 1,047 km/h)
Cruise speed: 442 kn (525 mph, 844 km/h)
Combat radius: 4,480 mi (3,890 nmi, 7,210 km)
Ferry range: 10,145 mi (8,764 nmi, 16,232 km)
Service ceiling: 50,000 ft (15,000 m)
Rate of climb: 6,270 ft/min (31.85 m/s)
Wing loading: 120 lb/ft² (586 kg/m²)
Thrust/weight: 0.31
Lift-to-drag ratio: 21.5 (estimated)
Armament
Guns: 1× 20 mm (0.787 in) M61 Vulcan cannon originally mounted
in a remote controlled tail turret on the H-model, removed from
all current operational aircraft in 1991
Bombs: Approximately 70,000 lb (31,500 kg) mixed ordnance;
bombs, mines, missiles, in various configurations
Avionics
Electro-optical viewing system that uses platinum silicide
forward looking infrared and high resolution low-light-level
television sensors
ADR-8 chaff rocket (1965-1970)[229]
LITENING Advanced Targeting System[266]
Sniper Advanced Targeting Pod[267]
IBM AP-101 computer[88]
HTML http://www.airforceworld.com/bomber/gfx/b52/b52_2.jpg
AC-130 Gunship
Crew: 13
Officers: 5 (pilot, copilot, navigator, fire control officer,
electronic warfare officer)
Enlisted: 8 (flight engineer, TV operator, infrared detection
set operator, loadmaster, four aerial gunners)
Length: 97 ft 9 in (29.8 m)
Wingspan: 132 ft 7 in (40.4 m)
Height: 38 ft 6 in (11.7 m)
Wing area: 1745.5 ft² (162.2 m²)
Loaded weight: 122,400 lb (55,520 kg)
Max. takeoff weight: 155,000 lb (69,750 kg)
Powerplant: 4 × Allison T56-A-15 turboprops, 4,910 shp (3,700
kW) each
Performance
Maximum speed: 260 knots (300 mph, 480 km/h)
Range: 2,200 nm (2,530 mi, 4,070 km)
Service ceiling: 30,000 ft (9,100 m)
Armament
4× 7.62 mm GAU-2/A miniguns
4× 20 mm (0.787 in) M61 Vulcan 6-barrel Gatling cannon
AC-130A Surprise Package, Pave Pronto, AC-130E Pave Spectre
2× 7.62 mm GAU-2/A miniguns
2× 20 mm M61 Vulcan cannon
2× 40 mm (1.58 in) L/60 Bofors cannon
AC-130E Pave Aegis
2× 20 mm M61 Vulcan cannon
1× 40 mm (1.58 in) L/60 Bofors cannon
1× 105 mm (4.13 in) M102 howitzer
AC-130H Spectre[60]
(Prior to c. 2000)
2× 20 mm M61 Vulcan cannon
1× 40 mm (1.58 in) L/60 Bofors cannon
1× 105 mm (4.13 in) M102 howitzer
(Current Armament)
1× 40 mm (1.58 in) L/60 Bofors cannon
1× 105 mm (4.13 in) M102 howitzer
AC-130U Spooky II
1× General Dynamics 25 mm (0.984 in) GAU-12/U Equalizer
5-barreled Gatling cannon
1× 40 mm (1.58 in) L/60 Bofors cannon
1× 105 mm (4.13 in) M102 howitzer
AC-130W Stinger II / AC-130J Ghostrider[24]
1x 30 mm ATK GAU-23/A autocannon[61]
1x 105 mm M102 Howitzer (AC-130J Ghostrider only, fired out the
back of the aircraft via a modified rear ramp.)[62][63]
'Gunslinger' weapons system with launch tube for AGM-176 Griffin
missiles and/or GBU-44/B Viper Strike munitions (10 round
magazines)[3]
Wing mounted, AGM-114 Hellfire missiles, GBU-39 Small Diameter
Bombs (SDBs) and/or GBU-53/B SDB IIs[3] (4 per hardpoint on
BRU-61/A rack)[64][65]
AvionicsEdit
AC-130H Spectre
Mission systems:
Northrop Grumman AN/APN-241 multimode navigation radar – derived
version of AN/APG-66 radar (formerly used on F-16A Fighting
Falcon) consisting of precised navigation and air-to-ground
modes including Monopulse Ground Mapping (MGM), Doppler Beam
Sharpening (DBS), high resolution Synthetic Aperture Radar
(SAR), Terrain Avoidance/Terrain Following (TA/TF), skin paint
(for Station KEeping; SKE), maritime detection,
weather/turbulence detection, wind shear alert, and ballistic
wind measurement (for precision airdrop)[66]
Motorola (now General Dynamics) AN/APQ-150 Beacon Tracking Radar
(BTR) – side-looking radar designed to search, acquire, and
track ground beacon signal (X-band transponder) located at a
friendly position from 10 nautical miles, beacon coordinate is
used as a reference point for ground troop to give the gunship a
bearing and range from the beacon to the desired target (mounted
between 40 mm cannon and 105 mm howitzer)[67][68]
Cubic Corporation AN/ARS-6 Personnel Locator System (PLS) –
radio navigation set[68]
Raytheon AN/AAQ-26 Infrared Detecting Set (IDS) – long-wave
infrared (LWIR) band Forward Looking Infrared (FLIR) (mounted
forward of the nose landing gear door)[68][69]
General Electric (now Lockheed Martin) AN/ASQ-145 Low Light
Level Television (LLLTV) – EO fire control system consists of
television camera (CCD-TV), AN/AVQ-19 Laser Target
Designator/Ranger (LTD/R – 1064 nm laser emitter with
permanently preset PRF code) with eyesafe mode (1570 nm laser
emitter), AN/AAT-3 Ambient Temperature Illuminator (ATI – wide
beam 860 nm laser illuminator), and Infrared Zoom Laser
Illuminator Designator (IZLID – airborne version of 860 nm
narrow beam laser pointer/marker and illuminator AN/PEQ-18)
(mounted in the crew entrance door)[67][68]
Navigation systems:
Teledyne Ryan (now Northrop Grumman) AN/APN-218 radar – doppler
navigation radar[68]
Previously installed systems:
AN/APN-59 radar – search and weather radar[68]
AC-130U Spooky II
Mission systems:
Raytheon AN/APQ-180 multimode attack radar – enhanced version of
AN/APG-70 radar (used on F-15E Strike Eagle) incorporating
several enhanced air-to-ground modes such as fixed target track,
ground moving target indication and track, projectile impact
point position, beacon track, and a weather
detection[68][70][71]
Raytheon AN/AAQ-26 IDS – LWIR FLIR (mounted on port side of the
nose landing gear door)[68][69]
Lockheed Martin AN/AAQ-39 Gunship Multispectral Sensor System
(GMS2) – EO/IR fire control system consists of mid-wave infrared
(MWIR) FLIR, two Image-Intensified Television (I2TV) cameras
(CCD-TV), laser target designator/rangefinder with eyesafe mode
(1064 and 1570 nm dual mode laser emitter), and near-infrared
(NIR) laser pointer/marker (860 nm laser emitter) (mounted under
the nose of port landing gear sponson)[72]
Previously installed systems:
GEC-Marconi All Light Level Television (ALLTV) – EO fire control
systems consists of CCD-TV, Laser Target Designator/Range Finder
(LTD/RF – 1064 nm laser emitter with in-flight programmable PRF
code) with eyesafe mode (1570 nm laser emitter), and Laser
Illuminator Assembly (LIA – 860 nm laser emitter)[68]
Countermeasures:
Raytheon AN/ALR-69 – digital Radar warning receiver
(RWR)[70][73]
L-3 Communications AN/AAR-44 – UV-based Missile Approach Warning
System (MAWS)[74]
ITT Exelis AN/ALQ-172 – Digital radio frequency memory (DRFM)
jammer-based Electronic countermeasure (ECM) incorporating
integrated Electronic Warfare (EW) self-protection function of
detection, processing, warning, prioritization, jamming, and
threat display[70][75]
BAE Systems AN/ALQ-196 Low-Band Jammer (LBJ) – low frequency
DRFM jammer-based ECM[76]
Northrop Grumman AN/AAQ-24 Nemesis – laser-based Directional
Infrared Counter Measures (DIRCM) (mounted on the port and
starboard rear fuselage)[77]
BAE Systems AN/ALE-47 Countermeasure Dispensing System (CMDS) –
chaff/flare dispenser[78]
HTML http://www.foro3d.com/attachments/122602d1265103639-blueprint-ac-130-a-ac-130.jpeg
#Post#: 2394--------------------------------------------------
Re: Gondor Factbook
By: Heavenly Paradise Date: June 24, 2015, 12:54 pm
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HTML http://orig08.deviantart.net/84f0/f/2008/125/b/b/clv_78_hauler_dropship_by_paintfan08.png
#Post#: 2626--------------------------------------------------
Re: Gondor Factbook
By: Heavenly Paradise Date: June 28, 2015, 3:38 pm
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HTML http://fc03.deviantart.net/fs70/f/2010/060/b/6/Colonial_Marines_UD4L_Cheyenne_by_bagera3005.png
Cheyenne Dropship
It acts as a gunship by using its own internal gun and deploying
weapon pods and hardpoints for rockets and missiles. The
principle airframe is constructed from superplastic-formed
diffusion-bonded metal matrix composites (MMC) and its 103.6
cubic meter internal payload bay can easily fit a M577 A.P.C.
(turret stowed). The engines can produce exceptionally high
thrust for low specific fuel consumption. The UD4L Dropship is
also called a "Cheyenne." It has AN/ALQ-2004E defensive systems
to keep it well protected. It has two types of power plants to
allow vertical take-off capability (VTOL) hover to the
hypersonic trans-atmospheric.
Crew: Pilot and Chief/Weapons Officer
Engines: 2 Republic Dynamics TF-900 turbines each rated at 310
kN dry thrust and 2 TF-220/A-14 combined cycle engines.
Dimensions Height: 6.05 m Length: 25.18 m Span: 12.59 m
Weights Loaded: 18,260 kg Maximum Loaded: 34,630 kg
Performance: Power to weight ratio (loaded) 1:3.3; (maximum
loaded) 1:1.7. Range is variable dependant on mission profile,
load and ambient atmospheric conditions, but the UD4L is capable
of dropping a load from low orbit, landing vertically, and
lifting to orbit again from a vertical launch.
Armament: 1 x 25 mm gatling gun with 900 rounds 32 x 150 mm
unguided rockets 12 x 70 mm unguided rockets 8 x 120 mm guided
rockets 7 x AGM-220 air-to-ground missiles 3 x TSAM threat
suppression missiles 3 x AIM-90 short range air-to-air missiles
#Post#: 2627--------------------------------------------------
Re: Gondor Factbook
By: Caos Date: June 28, 2015, 3:52 pm
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*pssst!* The dropship can't actually fly!
#Post#: 2770--------------------------------------------------
Re: Gondor Factbook
By: Heavenly Paradise Date: June 30, 2015, 2:11 pm
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Crew: Flight crew: 4 (pilot, copilot, navigator, flight
engineer)
Mission crew: 13–19
Length: 152 ft 11 in (46.61 m)
Wingspan: 145 ft 9 in (44.42 m)
Height: 41 ft 4 in (12.6 m)
Wing area: 3,050 ft² (283.4 m²)
Empty weight: 185,000 lb (73,480 kg)
Loaded weight: 344,000 lb (with aerial refueling) (156,036 kg)
Max. takeoff weight: 347,000 lb (157.397 kg)
Powerplant: 4 × Pratt and Whitney TF33-PW-100A turbofan, 21,500
lbf (93 kN) each
Performance
Maximum speed: 530 mph (855 km/h, 461 knots)
Range: 4,000 nmi (7,400 km) (8 hr)
Service ceiling: 41,000 ft (12,500 m)
HTML http://media-2.web.britannica.com/eb-media/71/130771-004-355D9D6A.jpg
#Post#: 3405--------------------------------------------------
Re: Gondor Factbook
By: Heavenly Paradise Date: July 6, 2015, 12:25 pm
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Anti-submarine plane
TU-142
Tu-142M
The Tu-142M is a long-range anti-submarine / reconnaissance
aircraft designed by the Tupolev Design Bureau and manufactured
by the Kuibyshev Aviation and Taganrog Machinery plants. The
aircraft is developed to provide improved naval combat
capabilities. It can be deployed primarily in anti-submarine
warfare (ASW) operations, maritime reconnaissance and low-range
patrol runs.
The aircraft is equipped with a set of anti-submarine weapons to
protect territorial waters from potential enemy submarines. The
aircraft have been in service with the Indian Navy's 312nd
squadron (INAS 312) since 1988 and are deployed in
anti-submarine warfare and patrol missions across the Indian
Ocean.
Tu-142M orders and deliveries
Tupolev Design Bureau received an executive order to design and
develop the Tu-142 aircraft, which is based on the long-range
Tu-95 turboprop strategic bomber. The prototype aircraft was
built at Kuibyshev Aviation Plant and made its first flight in
June 1968. The first aircraft entered trail operation with the
Soviet Naval Aviation in May 1970 and was officially
commissioned into service in December 1972.
"The aircraft is equipped with a set of anti-submarine weapons
to protect territorial waters from potential enemy submarines."
The first modernised Tu-142M aircraft equipped with advanced
avionics performed its maiden flight in 1985. Eight Tu-142Ms
(IN-311 to IN-318) in export version (Tu-142ME) were built
between 1987 and 1988 at the Taganrog Aviation Plant (now TAVIA)
for the Indian Navy. The aircraft were commissioned in 1988.
In 2006 and 2007, two of the Tu-142M aircraft operated by the
Indian Navy were upgraded by TAVIA, a division of Beriev
Aircraft Company. Two more aircraft were retrofitted in July
2010.
The Indian Navy received seventh modernised Tu-142ME (IN 317)
aircraft in August 2014.
Tu-142M design and features
The Tu-142M anti-submarine aircraft features monoplane, mid-wing
design. It is fitted with a single-fin tail and tricycle landing
gear with controlled front wheels. It features a monocoque
fuselage, which has a length of 46.4m and a maximum diameter of
2.9m.
The fuselage incorporates a set of longitudinal stringers,
cross-set of frames with stressed skin. Two cargo compartments
are located at the lower part of the fuselage. The tail section
is fitted with a rear cannon mounting. The nose cone section is
installed with an in-flight refuelling system. A hatch is
located in the niche of the front leg to facilitate emergency
access.
The aircraft is roughly 49.5m in overall length, 12.12m high and
has wing span of approximately 50m. It has a maximum takeoff
weight of 185,000kg and is operated by a crew of 11, including
flight crew and navigators / observers.
The aircraft is armed with a variety of defensive weapons such
as Kh-35 anti-ship missile, self-guided missiles, twin AM-23
automatic cannon, depth charges and torpedoes.
Sensors on-board Tu-142M
The Tu-142M anti-submarine aircraft is equipped with DRDO HOMI
airborne electronic support measures system to identify, locate
and detect enemy targets. It incorporates Korshun-K integrated
automatic search and targeting system and MMS-106 Ladoga
magnetometer to detect nuclear-powered submarines.
The aircraft is also fitted with a Strela onboard communication
system, a NPK-142M navigation system, a Sayany onboard defence
system and a Nerchinsk hydrological defence system. The
sonobuoys incorporated in the aircraft include RGB-15, RGB-25
and RGB-55A.
Engines and performance
The Tu-142M anti-submarine aircraft is powered by four NK-12M
turboprop engines designed by the Kuznetsov Design Bureau. Each
engine develops a power output of 15,000shp. The propulsion
system also consists of four coaxial eight-bladed
reversible-pitch propellers. The aircraft has a fuel capacity of
87,000kg.
The operational speed of the aircraft is 442mph, while the
maximum speed is 574.76mph at high altitudes. The operating
range of 3,977mi and the maximum range is 7,953.55mi. The
service ceiling of the aircraft is 39,000ft.
The plane also has a MAD detector under the nose, with a seven
meter boom. The payloads of this aircraft can include sonobuoys,
torpedoes, depth charges, anti ship missiles, and drop bombs
with a payload of 20,000 pounds.
HTML http://warfare.be/0702ey70/update/january2009/tu-142.jpg
#Post#: 3664--------------------------------------------------
Re: Gondor Factbook
By: Heavenly Paradise Date: July 7, 2015, 5:19 pm
---------------------------------------------------------
Crew: 1
Length: 62 ft 1 in (18.92 m)
Wingspan: 44 ft 6 in (13.56 m)
Height: 16 ft 8 in (5.08 m)
Wing area: 840 ft² (78.04 m²)
Airfoil: NACA 64A?05.92 root, NACA 64A?04.29 tip
Empty weight: 43,340 lb (19,700 kg)
Loaded weight: 64,840 lb[250] (29,410 kg)
Max. takeoff weight: 83,500 lb (38,000 kg)
Powerplant: 2 × Pratt & Whitney F119-PW-100 pitch thrust
vectoring turbofans
Dry thrust: 26,000 lb[250] (116 kN) each
Thrust with afterburner: 35,000+ lb (156+ kN) each
Fuel capacity: 18,000 lb (8,200 kg) internally, or 26,000 lb
(12,000 kg) with two external fuel tanks
Performance
Maximum speed:
At altitude: Mach 2.25 (1,500 mph, 2,410 km/h) [estimated][106]
Supercruise: Mach 1.82 (1,220 mph, 1,960 km/h)[106]
Range: >1,600 nmi (1,840 mi, 2,960 km) with 2 external fuel
tanks
Combat radius: 410 nmi (with 100 nmi in supercruise) (470 mi,
760 km)
Ferry range: 2,000 mi (1,740 nmi, 3,220 km)
Service ceiling: >65,000 ft (20,000 m)
Wing loading: 77.2 lb/ft² (377 kg/m²)
Thrust/weight: 1.08
Maximum design g-load: −3.0/+9.0 g[106]
Armament
Guns: 1× 20 mm (0.787 in) M61A2 Vulcan 6-barrel Gatling cannon
in right wing root, 480 rounds
Air to air loadout:
6× AIM-120 AMRAAM OR 6x Meteor MS20
2× AIM-9 Sidewinder
Air to ground loadout:
2× 1,000 lb (450 kg) JDAM or 8× 250 lb (110 kg) GBU-39 Small
Diameter Bombs
2× AIM-120 AMRAAM
2× AIM-9 Sidewinder
Hardpoints: 4× under-wing pylon stations can be fitted to carry
600 U.S. gallon drop tanks or weapons, each with a capacity of
5,000 lb (2,270 kg).[251]
Avionics
AN/APG-77 radar: 125–150 miles (200–240 km) against 1 m2 (11 sq
ft) targets (estimated range)[109]
AN/AAR-56 Missile Launch Detector (MLD)[86]
AN/ALR-94 radar warning receiver (RWR): 250 nmi (463 km) or more
detection range[117]
MJU-39/40 flares for protection against IR missiles[252]
[img]
HTML http://vignette3.wikia.nocookie.net/aircraft/images/1/1b/F22_specs.jpg/revision/latest?cb=20101025041426[/img]
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