Showing posts with label AIRCRAFT. Show all posts
Showing posts with label AIRCRAFT. Show all posts

Sunday, March 27, 2011

The Sukhoi T-50




The Cold War was over but the ever-continuing race for space supremacy doesn’t mean to end. Allied or opposing nations may come in terms to agree with each other on common grounds but deep inside each will have the self reservation to secure their individual interests should any eventuality arise that each must face each other on the battlefield for a conflict of interests that couldn’t be resolved on the bargaining table. As history repeats itself, mankind will have to forget the lessons it learned through hard times of lives lost and edifices destroyed in acts of war for the same reason, insecurity .

Keeping in circulation to adapt to the call of the times, Russia just need to keep up with the west in pursuing her strategic capabilities as a once powerful nation. The state of worldwide economy just seems to make everything unstable and with it comes the worst possibilities which could be expected.

The Sukhoi T-50 PAK-FA (Perspektivny aviatsionny kompleks frontovoy aviatsii) or “"Future Frontline Aircraft System" in literal translation is a 5thgeneration jet-fighter developed by Sukhoi for the Russian Air Force. By the status of the program, it was meant to compete with the US built Lockheed-Martin F-22 Raptor and the F-35 Lightning II. Russia’s Sukhoi and India’s HAL (Hindustan Aeronautics Limited) has joined forces for building two variants of this aircraft, a single-seater of about 200 units and a twin-seater of about 50 units for Russian Air Force with 200 twin-seater units and 50 single-seater variants for the Indian Air Force.

he Soviet Union’s need to replace the fleet of Mig-29 Fulcrums and Su-27 Flankers came about in the late 80’s which were met with two options, the Sukhoi Su-47 Berkut and the Mikoyan Project 1.44. Sukhoi won the contract of developing the new combat aircraft in 2002 and the design for a prototype was approved in 2009 which integrates both technologies from the Su-47 and the Mikoyan Project 1.44. The first prototype took to the skies in January 2010 out of the 3 built. Information on the fighter was highly classified however photographs taken of the prototype reveals its striking similarity with the US built F-22 Raptor which incorporates both stealth and supercruise capabilities thus it is assumed that the Russian fighter itself features the same strong points.

Performance Specifications based on data from Warfare.Ru

Performance

* Maximum speed:Mach 2.45 (3,000+ km/h, 1,850+ mph)
* g-limits:(9 g)
* Cruise speed:1,800 km/h (1,100 mph)
* Ferry range:4,000 to 5,500 km (2,500 to 3,400 mi)
* Service ceiling:20,000 m (65,617 ft)
* Rate of climb:350 m/s (68,898 ft/min)
* Wing loading:470 kg/m² (96.3 lb/ft²)
* Thrust/weight:1.4 (dry thrust)
* Runway:350 m (1,148 ft)
* Endurance:3.3 hrs (198 mins)

Saturday, March 26, 2011

F-117A Nighthawk




The Lockheed F-117A "Stealth" fighter in one of the most sophisticated warplanes ever built, almost invisible to radar, the F-117 has revolutionized air warfare.
At first, the aircraft was operated under conditions of total secrecy, but during the US intervention in Panama in 1990 and during the first Gulf War in 1991 the U.S. Air Force deployed it openly.

In 1974, the US Defense Advanced Research Projects Agency (DARPA) initiated a program known as PROJECT HARVEY, after a well-known comedy about an invisible giant rabbit, that requested designs of an "experimental survivable testbed (XST)" aircraft with a low RCS. Lockheed was not among the companies contacted by DARPA with this request, but in 1975 Ben Rich, an engineer who had worked on the secret Lockheed U-2 and SR-71 reconnaissance aircraft, got wind of the project and lobbied the government successfully to have Lockheed included.

Rich had the services of two Lockheed employees, mathematician Bill Schroeder and computer scientist Denys Overholser, to work on the XST program. Schroeder realized that it would be much easier to compute RCS if the shape of an aircraft could be reduced to a set of flat surfaces, or "facets". Schroeder approached Overholser with the idea, and within five weeks Overholser had written a computer program named "Echo I" that could determine the RCS of a "faceted" aircraft. Armed with Echo I, Schroeder came up with an initial XST design that he called the "Hopeless Diamond", and handed Ben Rich a sketch of it in May 1975.
In response, Rich asked how big the RCS of a practical version of the Hopeless Diamond would be: As big as a T-33? A Piper Cub? A condor? An eagle? An owl? Schroeder shot back: "Ben, try as big as an eagle's eyeball."

By October 1975, the DARPA XST competition had been reduced to two finalists: one from Northrop, and a refined version of the Lockheed Hopeless Diamond. The Northrop entry was a delta with a faceted fuselage, with the jet engine mounted on the back and the intake above the cockpit.
The Lockheed design had a tenth of the RCS of the Northrop design. It was so invisible to radar that a radar operator performing tests on the model at White Sands, New Mexico, thought it had fallen off the pole. Bird droppings increased the RCS by 50 percent, and so the model had to be regularly cleaned. Lockheed won the competition in April 1976. The Northrop team was heartbroken, even though their engineers admitted Lockheed had the better design. They returned to their calculations and would eventually catch up with Lockheed at the stealth game, with the B-2 Spirit bomber.
Have Blue

When the Carter Administration took office in early 1977, Bill Perry, an influential defense undersecretary for research and engineering and later defense secretary in the Clinton Administration, learned of how dramatic the results of the model tests had been. Perry immediately saw to it that program became secret. Responsibility was transferred from the mostly-civilian DARPA to the USAF Special Projects Office, and funding was increased. Orders went out stating that the word "stealth" was not be used in unclassified documents, and the program was assigned a meaningless two-word codename: HAVE BLUE.

The first of the two HAVE BLUE demonstrators was intended for aerodynamic tests. Faceting had an interesting consequence: unlike almost every other aircraft ever built, HAVE BLUE's wings did not have a curved cross-section, being composed instead of flat planes. Its aerodynamics were suspicious, and in fact the machine was so unstable that it had to be controlled by a computerized fly-by-wire system. The first prototype was needed to ensure that the design could fly at all. The second would be a more finished product that would be used for stealth demonstrations.

The HAVE BLUE prototypes were 17.25 meters (38 feet) long, with a wingspan of 10.2 meters (22.5 feet) and a weight of 5.67 tonnes (12,500 pounds). Each was powered by a pair of General Electric J85-GE-4A engines with 13.1 kN (1,340 kgp / 2,950 lbf) each, obtained from Navy T-2B Buckeye trainers. Other scavenged equipment included the fly-by-wire system, modified from the F-16A fighter; and ejection seat, landing gear, and cockpit instrumentation taken from an F-5 fighter.
Senior Trend

The Air Force was impressed by the flight tests of the HAVE BLUE 1001 test aircraft, and in mid-1978 Lockheed suggested two designs for an actual weapons system: a medium bomber with four engines and a two-man crew, and a single-seat twin-engine strike fighter. The Air Force preferred the strike fighter concept, and issued a design contract to Lockheed for such an aircraft in November 1978. The aircraft was given the code name 'Senior Trend'.

The Senior Trend aircraft was a direct outgrowth of the HAVE BLUE prototypes, with many changes to turn the design into a practical combat aircraft. HAVE BLUE's wings had a sharp sweep of 72.5 degrees, which gave it the flatiron flight characteristics that had led to the loss of the first prototype. As a result, the sweep of Senior Trend's wings was reduced to 67.5 degrees, and the wings were extended as far back as possible.

Senior Trend was about twice as big as HAVE BLUE. It was 20 meters (65.9 feet) long, with a wingspan of 13.2 meters (43.25 feet), and an empty weight of 13.6 tonnes (30,000 pounds). The canopy was heavily framed and had poor visibility. The mid-air refueling receptacle was positioned behind the cockpit. The door over the receptacle had serrated edges to reduce radar reflection, as did the landing gear doors and canopy leading edge.

Senior Trend was mostly built out of aluminum, though titanium was used around the engines. It was powered by twin General Electric F404-GE-F1D2 turbofans, like those of the F/A-18 Hornet fighter but without afterburners, providing 48.1 kN (4,900 kgp / 10,800 lbf) thrust each. The intakes were covered by grilles, which were electrically heated to prevent them from icing up. The pilot could also activate lights on either side of the cockpit to allow him to check the intake grilles for icing.

The first production aircraft, number 785, was delivered to Groom Lake in the spring of 1982. It crashed and was destroyed on take-off on 20 April, badly injuring the pilot, Bob Ridenauer of Lockheed, who never flew again. The accident was traced to reversed wiring in the flight control system. Number 786 was delivered to Groom Lake in June and used for flight testing.

Senior Trend 787 was the first of the black aircraft to be flown by the 4450th Tactical Group, making its first operational flight on 15 October 1982. By Christmas, several more Senior Trend's had been delivered to TTR, and the F-117A Nighthawk, as the aircraft had been formally named, was in business.
F-117A Nighthawk

As the F-117s trickled into Tonopah, operations evolved into a schedule. Flight crews were shuttled there each Monday afternoon on a chartered airliner from Nellis Air Force Base, after spending the weekend home with their families. On arriving at Tonopah, they would be given a briefing on the night's mission.

Hangar doors were not opened until an hour after dark. For the first year of operations, flight operations were restricted to the Nellis range. Permission to perform off-range operations had to be given by the President himself. Flight routes were defined to avoid populated areas, and some routes were not used if the Moon was more than 50% full. Pilot communications and transponder signals were defined so that the aircraft mimicked an A-7.

Training flights were conducted in two waves, one early and one late in the night. The missions simulated precision strikes on local targets, such as the crossroads of two dirt roads or a shanty in the wilderness. The missions ended before sunrise, since it was found that a pilot found it hard to go to sleep if he went to bed after sunrise.

The enthusiasm for the F-117 grew to the point where the Air Force wanted more of them. The original plan had been for a single squadron of 18 aircraft, organized for special operations, but the plan was expanded to an entire wing, with three 18-aircraft squadrons. Lockheed would build a total of 59 production F-117s, with the second squadron activated in July 1983, and the third going into operation in October 1985. A total of over $6 billion USD would be spent building the F-117s.
Desert Storm

During Operation Desert Storm F-117's were stationed at King Khaled Air Base in Saudi Arabia. Their new home was at the southern tip of Saudi Arabia, well out of range of Iraqi Scud tactical ballistic missiles, and was well-equipped with hardened shelters. It became known as "Tonopah East", with the similarities in environment possibly being a factor in the selection of the name. The F-117 pilots soon began an intensive training program, since few of the pilots had combat experience in any sort of aircraft.

On 12 January 1991, the US Congress voted to allow the use of force to remove the Iraqis from Kuwait, in support of a UN resolution demanding that Saddam pull out of the country. On 15 January, the deadline specified by the UN resolution expired. The next day, F-117 pilots were briefed for their strikes. During the operation, the 40 assigned F-117's flew almost 1,300 combat sorties. They dropped almost 2,000 tons of bombs, during 6,900 flight hours.
Retirement

In February 2006, the Pentagon proposed to speed up retirement of the F-117 Nighthawk and U-2 spy plane to save about $2 billion. To make room for the new F-22 Raptor stealth fighter, and the unmanned reconnaissance drone RQ-4 Global Hawk, the Pentagon wil retire all 52 F-117s in 2008 and the U-2s by 2011.

Mig-29 Fulcrum




Mig-29 Fulcrum Specifications
Version Mig-29 Fulcrum
Manufacturer(s) Mikoyan-Gurevich
Country Russian Federation/ USSR
Role Multi-role fighter
Powerplant Klimov RD-33K turbofan engine (2x)
Thrust 86.4kN 19,400 lbs (with afterburner)
Length 17.37m 57ft
Height 4.73m 15.6 ft
Wingspan 11.4m 37.3ft
Weight 11,000kg 24,250 lbs (empty)
Speed 2,430km/h 1,510mph
Range n/a
Ceiling 17,000m 55,800ft
Crew 1
First deployment n/a
Cost n/a


The MiG-29 is a widely exported aircraft, flown by Russia, Bulgaria, Croatia, Cuba, Czech Republic, Germany, Hungary, India, Iran, Iraq, Kazakhstan, Malaysia, Moldova, North Korea, Poland, Romania, Slovakia, Syria, Turkemenistan, Ukraine, Uzbekistan, Yemen and Yugoslavia.
In total, over 800 were delivered to the Soviet / Russian Tactical Air Forces and around 500 airframes prepared for initial export customers.
By 1989, it was serving in 12 different air forces around the world.
Presently, it is the only Russian aircraft on operational duty in NATO and serves in 21 air forces.
Brassey's reports that a total of 1216 MiG-29 single-seaters and 197 MiG-29UB dual-seaters were built by January 1985 (total of 1413). Since 1990, production was exclusively for export.

The MiG-29 has a few advantages over its more electronically advanced American counterparts. At about 40 miles apart, the American planes have the advantage because of avionics. At 10 miles the advantage is turning to the MiG. At five miles out, because of the MiG weapons sight and better maneuverability, the advantage is to the MiG.
The mission of the MiG-29 is to destroy hostile air targets within radar coverage limits and also to destroy ground targets using unguided weapons in visual flight conditions.
The aircraft's fixed-wing profile with large-wing leading-edge root extensions gives good manoeuvrability and control at subsonic speed, including manoeuvres at high angles of attack. The maximum operational g-loading is 9g.

The MiG29B was designed later on as a two-seated combat trainer. There is also a MiG29C with extended fuel capacity, of the 21 Fulcrums the United States bought, 14 are the frontline Fulcrum C's, which also contains an active radar jammer in its spine, six Mig 29A versions and one B-model of training.
During 1989 and 1990 a naval version was also under testing under the name MiG29D.

The latest version of MiG29 is the Super Fulcrum, MiG29K. The MiG-29K differed from the MiG-29 production model, featuring a new multi-function radar.
It is a highly improved MiG29, but unfortuately it hasn't been produced in great numbers.
The aircraft has a remote control system, large-area (42 m2 vs 38 m2) folding wing, adjustable center-line air intakes with retractable screens protecting the engines during operation from ground airfields, reinforced landing gear, hook, corrosion- protected reinforced fuselage made specifically for deck-based aircraft.

The German 'Bundeswehr' inherited 20 single-seater and 4 twin-seater MiG-29 aircraft from the former East German forces after the cold war.
After these Fulcrum aircraft had been upgraded to western standards, they received the designations MiG-29G (for Germany) and MiG-29GT (Germany/Trainer).

The MiG-29 fighter is equipped with seven external weapon hardpoints.
The aircraft can carry: up to two R-27 air-to-air medium-range missiles; six R-73 and R-60 air-to-air short range missiles; four pods of S-5, S-8, S-24 unguided rockets; air bombs weighing up to 3,000kg; and 30mm built-in aircraft gun with 150 rounds of ammunition.

During the NATO actions in Kosovo, on the 24th of March 1999, a Dutch F-16 shot down a Serbian Mig-29.

Armament:

# One 30mm GSh-30L cannon with 150 rounds
# Six Air-Air Missiles; including a mix of SARH and AA- 8 Aphid (R60) AA-10 Alamo (R27T) AA-11 Archer (R73) FAB 500-M62, FAB-1000, TN-100,
# ECM Pods
# S-24 AS-12, AS-14
Versions:

* Mig-29 " Fulcrum-have ": Basical version. Feature: to see above.
* Mig-29UB " Fulcrum-Bs ": Two-seater Training version.
* Mig-29S " Fulcrum-Cs ": Modernized version of Fulcrum-H.
* Mig-29SE: Export version of export of the Fulcrum-C.
* Mig-29K " Fulcrum-Ds ": Aircraft Carrier based version of the Mig-29. (based on Kusnetzov Carrier)
* Mig-29M: Last version of the Mig-29, completely revisited.
* Mig-29ME: Export Version of the Mig-29M.
* Mig-29G: German upgraded version
* Mig-29GT: German upgaded two-seater trainer

Thursday, March 24, 2011

F-22 Raptor




The Lockheed Martin YF-22 won the Air Force's Advanced Tactical Fighter (ATF) contest over the Northrop YF-23 in April 1991. In 1983 the Air Force had issued a request for proposals for the ATF program, which were based on a study on new fighter concepts. The F-22 program is developing the next-generation air superiority fighter for the United States Air Force to ensure it retains it's air dominance and can counter emerging worldwide threats.
Two prototypes of both the YF-22 and YF-23 were constructed, one demonstrator of each aircraft being powered by Pratt & Whitney F119 and the other by the General Electric F120 turbofan engine, allowing the Air Force to select the best airframe/propulsion arrangement.
The second YF-22 prototype, fitted with the Pratt & Whitney engines, demonstrated the ability to cruise at Mach 1.58 without afterburner and Mach 1.7 with afterburner.
This combination was deemed the most desirable and both Lockheed and Pratt & Whitney were issued contracts to proceed with production. The first F-22 fighter aircraft was unveiled in April 1997 and was given the name Raptor.

The end of the Cold War greatly reduced the perceived military threat faced by the United States, therefore the House Appropriations Committee recommended termination of the F-22, based in part on concerns over cost growth and unrealistic budgeting.
The Air Force told the Committee that development of the then called ATF would cost around $14 billion, already 900 million dollars more than estimates provided half a year earlier.
In the years that followed the costs continued to rise, and was estimated at $23 billion in 1999.

Dispite the cost overruns and cuts in the total number of aircraft that will be purchased, the F-22A Raptor achieved Initial Operational Capability, and passed its 'mission capable' flight test in mid-January 2006.

In late-February Gen. Ronald Keys, commander of Air Combat Command (ACC), revised plans to procure a fleet of 183 Raptors, and will give the service about 126 combat-ready jets.

The Raptor's twin Pratt & Whitney F119-PW-100 engines are leading-edge powerplants. The F-119's ability to provide supersonic cruise without afterburner provides the F/A-22 with one of its most important capabilities, with supercruise at Mach 1.5+ demonstrated in flight tests. It has a high power-to-weight ratio (PWR) of 1.4:1, and can deliver 156 kN (15,900 kgp / 35,000 lbf) afterburning thrust. The F119 has a minimized parts count and has been designed for maintainability. Important components, harnesses, and plumbing were placed on the bottom of the engine to improve ground crew access, and all components can be removed or replaced with one of six standard tools. The digital engine control modules are redundant, with two controllers per engine and two computers per controller, to improve reliability.

The F/A-22 is constructed of titanium alloys (39% by weight); composites (24%); aircraft aluminum alloy (16%); and thermoplastics (1%). Advanced titanium welding techniques and composite fabrication are used in the aircraft's construction. "Radar absorbent material (RAM)" is used in critical locations to reduce the aircraft's radar signature, and the aircraft's contours are intended to make it less conspicuous to radar. Apertures, such as weapons bay and landing gear doors, have zigzag edges to break up radar returns. A overall coating reduces the aircraft's infrared signature as well. While older stealth aircraft require substantial maintenance, careful handling, and protection from weather to keep them stealthy, the F/A-22 will not require extraordinary efforts to maintain its stealth characteristics.