Tuesday, September 15, 2009

Lockheed Martin / Boeing F-22 Raptor


The Lockheed Martin/Boeing F-22 Raptor is a 5th generation Aircraft. The F-22 is the only fighter capable of simultaneously conducting air-to-air and air-to-ground combat missions with near impunity. In addition to being America’s most prominent air-superiority fighter, the F-22 evolved from its original concept to become a lethal, survivable and flexible multimission fighter. By taking advantage of emerging technologies the F-22 has emerged as a superior platform for many diverse missions including intelligence gathering, surveillance, reconnaissance and electronic attack.


Features of F 22 Raptor

• Advanced stealth – enables 24/7 operations while remaining virtually undetected by enemy forces
• Supercruise speeds greater than Mach 1.5 without afterburners – enhance survivability/lethality
• Extreme fighter agility – allows outmaneuvering through acceleration and razor-sharp turns
• Information fusion – generates 360-degree battlespace awareness for pilot
• Joint force enabler – assures future air dominance for joint and coalition forces


Variants:
Under the Navy Advanced Tactical Fighter (NATF) program, a carrier-borne variant of the F-22 with swing-wings was proposed for the U.S. Navy to replace the F-14 Tomcat, though the program was subsequently cancelled in 1993. A two-seat F-22B trainer variant was planned, but was cut in 1996 to save development costs. Another more recent proposal is the FB-22, which would be used as a deep strike bomber for the USAF, but there has yet to be any word on whether the USAF plans further development of the program. The FB-22 was projected to carry up to 30 Small Diameter Bombs to about twice the range of the F-22A, while maintaining the F-22's stealth and supersonic speed.

Product Life Cycle:


By 1990 Lockheed Martin, teamed with Boeing and General Dynamics, had built and flown the demonstration prototype aircraft, designated YF-22. The first F-22 fighter aircraft was unveiled in April 1997 and was given the name Raptor. In September 2002, the USAF decided to redesignate the aircraft F/A-22 to reflect its multi-mission capability in ground attack as well as air-to-air roles. The aircraft's designation was changed again to F-22A when it achieved initial operating capability (IOC) in December 2005. The decision to proceed to low-rate initial production (LRIP) was authorised in August 2001 and Lockheed Martin delivered 49 aircraft under LRIP contracts. Initial operational test and evaluation began in April 2004 and was successfully completed in February 2005. A further 60 Raptors were ordered in July 2007, bringing the total ordered to 183, with production to 2011. In November 2008, funding for four additional raptors was approved, increasing the total ordered jets to 187, with the buying scheduled in the second half of the fiscal year 2009. The USAF has a total requirement of 243 aircraft but funding was not made available for more than 187. By July 2008, 122 aircraft had been delivered. Holloman AFB is expected to deliver another 40 aircraft by the end of 2010.

Unit Cost US$142.6 million (2009 flyaway cost)


Specifications:

Dimensions:
Length: 62.07ft (18.92m)
Width:44.49ft (13.56m)

Height: 16.47ft (5.02m)

Structure:

Accommodation: 1
Hardpoints: 4 External and 8 Internal Hardpoints
Empty Weight: 31,998lbs (14,514kg)
MTOW: 54,999lbs (24,947kg)

Performance:

Max Speed: 1,599mph (2,574kmh; 1,390kts)

Max Range: 2,000miles (3,218km)
Rate-of-Climb:0ft/min (0m/min)
Service Ceiling: 50,000ft (15,240m; 9.5miles)


Powerplant:

Engine(s): 2 x Pratt & Whitney F119-PW-100 afterburning turbofans generating 35,000lbs of thrust each.

Armament Suite:

1 x 20mm Cannon 4 x AIM-9 Sidewinders (side weapon bays)
4 x AIM-120A Amraams (internal ventral bay)

6 x AIM-120Cs (internal ventral bay)
6 x GBU-32 JDAM PGMs (internal ventral bay)
8 x GBU-39 Small Diameter Bombs (250lbs ea)
4 x underwing hardpoints with a maximum of 5,000lbs (2,270kg) of mission-specific weaponry or fuel droptanks.

To know more about F- 22 Raptors please visit

http://www.militaryfactory.com/aircraft/detail.asp?aircraft_id=20
http://www.airforce-technology.com/projects/f22/
http://www.lockheedmartin.com/products/f22/f-22-capabilities.html

Wednesday, September 2, 2009

Mikoyan MiG-35 (Fulcrum-F)


The MiG-35 is "4++" generation multi-role fighter, exhibiting the further development of the MiG-29K/KUB and MiG-29M/M2 fighters in the field of the combat efficiency enhancement, universality and operational characteristics improvement.



Main features of MiG-35/MiG-35D:

· The fifth generation information-sighting systems integration into aircraft airborne avionics.

· Possibility of advanced Russian and foreign origin weapons application.

· Increased combat survivability due to integration of airborne integrated defense system.

· Air superiority gaining against four & fifth generation fighters.

· Interception of existing and being developed air attack means.

· Ground/surface targets destruction with high precision weapons without entering the air defense zone day and night in any weather conditions.


·The OLS on the MiG-35 is considered to help pilots to spot even the USAF's stealth planes.



Variants:

The fighter plane is being marketed globally under the designation MiG-35 (single seat) and MiG-35D (dual seat).


Product Life Cycle:

The final version of MiG-35 was displayed for the first time at Aero India 2007.



Unit cost $127.3 million


Specifications:

Dimensions:

Length: 62.34ft (19.00m)
Width:49.21ft (15.00m)
Height: 19.69ft (6.00m)

Structure:

Accommodation: 1 or 2
Hardpoints: 8
Empty Weight: 38,581lbs (17,500kg)
MTOW: 65,477lbs (29,700kg)

Performance:

Max Speed: 1,588mph (2,556kmh; 1,380kts)
Max Range
: 1,243miles (2,000km)
Rate-of-Climb:65,000ft/min (19,812m/min)
Service Ceiling: 62,008ft (18,900m; 11.7miles)

Powerplant:

Engine(s): 2 x Klimov RD-33K turbofan engines developing 19,840 lbf each with afterburn capable.

Armament Suite:

1 x 30mm GSh-30-1 cannon

OPTIONAL:
4 x AA-10 Alamo air-to-air missiles (R-27R, R-27T, R-27ER, R-27ET)

4 x AA-8 Aphid air-to-air missiles

8 x AA-11 Archer air-to-air missiles (R-73E, R-73M, R-74M)

8 x AA-12 Adder air-to-air missiles

4 x AS-17 Krypton anti-radiation missiles (Kh-31A, Kh-31P)

4 x AS-14 Kedge (Kh-29T, Kh-29L) air-to-surface missiles

4 x AS-20 anti-ship missile

S-24 unguided/laser-guided rockets

S-25L unguided/laser-guided rockets

S-250 unguided/laser-guided rockets

S-13 unguided/laser-guided rockets

S-8 unguided/laser-guided rockets

KAB-500L laser-guided bombs

KAB-500T TV-guided bombs

FAB-250 drop bombs

FAB-500 drop bombs

ZAB-500 fuel-air explosive bombs

Tuesday, September 1, 2009

Boeing / McDonnell Douglas / Northrop F/A-18 Super Hornet

The F/A-18 Hornet, an all-weather aircraft, is used as an attack aircraft as well as a fighter. In its fighter mode, the F/A-18 is used primarily as a fighter escort and for fleet air defense; in its attack mode, it is used for force projection, interdiction and close and deep air support.



Features of F/A-18 Super Hornet

The F/A-18E/F aircraft are 4.2 feet longer than earlier Hornets, have a 25% larger wing area, and carry 33% more internal fuel which will effectively increase mission range by 41% and endurance by 50%.

It has an all-weather air-to-air radar and a control system for accurate delivery of conventional or guided weapons

The F/A-18 has a digital control-by-wire flight control system which provides excellent handling qualities, and allows pilots to learn to fly the airplane with relative ease. At the same time, this system provides exceptional maneuverability and allows the pilot to concentrate on operating the weapons system.

A solid thrust-to-weight ratio and superior turn characteristics combined with energy sustainability, enable the F/A-18 to hold its own against any adversary.


Variants:

F/A-18E Super Hornet: single seat variant

F/A-18F Super Hornet: two-seat variant

EA-18G Growler: The electronic warfare version of the F/A-18F Super Hornet, slated to begin production in 2008, with fleet deployment in 2009. The EA-18G will replace the U.S. Navy's EA-6B Prowler.


Product life cycle:

The US Navy F/A-18 E and F Super Hornet maritime strike attack aircraft, manufactured by Boeing, flew for the first time on November 29 1995.

The first low-rate initial production aircraft was delivered in December 1998, and all 12 of the first batch were delivered by November 1999. In February 1999, the US Navy placed an order for 30 Super Hornets, in addition to the 12 already ordered. Following successful completion of operational evaluation, in June 2000 the USN ordered 222 fighters to be produced over the next five years.

The first full-rate production aircraft was delivered in September 2001. Over 200 aircraft have been delivered.

A second multi-year contract was signed in January 2004 for 42 aircraft to be purchased between 2005 and 2009. Total requirement is for at least 545 aircraft.

Unit cost US$54.7 million

Specifications:

Dimensions:

Length: 60.07ft (18.31m)
Width:44.69ft (13.62m)
Height: 16.01ft (4.88m)

Structure:

Accommodation: 1 or 2
Hardpoints: 11
Empty Weight: 30,565lbs (13,864kg)
MTOW: 47,003lbs (21,320kg)

Performance:

Max Speed: 1,187mph (1,911kmh; 1,032kts)
Max Range
: 680miles (1,095km)
Rate-of-Climb: classified
Service Ceiling: 49,213ft (15,000m; 9.3miles)

Powerplant:

Engine(s): 2 x General Electric F414-GE-400 turbofan engines generating 22,000lbs of thrust with afterburner.

Armament Suite:

1 x 20mm cannon

Mission-specific ordnance limited up to 17,750lbs may include any of the following:

AIM-9 Sidewinder air-to-air missiles

AIM-120 AMRAAM - air-to-air missiles

AGM-84 Harpoon anti-ship missiles
AGM-84E SLAM

AGM-88 HARM anti-radiation missiles

SLAM-ER

AGM-65 Maverick air-to-surface missiles

LAU Multiple Rocket Launcher

AGM-154 JSW (Joint Standoff Weapon) bombs

Joint Direct Attack Munition (JDAM) bombs

B61 Nuclear Dumb Bomb

Paveway Laser-Guided Bombs (LGB)

Mk 80 General Purpose Bombs

Mk-20 Rockeye II Cluster Bombs

Mk 20 CBU Cluster Bombs