Here is a link where you can find Yak-141 pictures
http://www.studenten.net/customasp/axl/plane.asp?cat_id=6&ple_id=67&page=0
Yak-141 Freestyle
http://www.globalsecurity.org/military/world/russia/yak-141.htm
The Yak-141 (formerly Yak-41) was intended originally to replace Yak-38 for air defence of
Kiev class carriers/cruisers, with secondary attack capabilities. Designed for carrier-borne operations as an air interceptor, close air combat, maritime and ground attack aircraft, the Yak-141 has the same multi-mode radar as the MiG-29, although with a slightly smaller antenna housed in the nose radome. It features a triplex full authority digital fly-by-wire system.
The Yak-141 continues previous Soviet V/STOL principles, combining a lift and propulsion jet with two fuselage mounted lift jets in tandem behind the cockpit, with cruise power provided by a single Tumansky R-79 jet engine. The R-79 has a rear lift/cruise nozzle which deflect down for take-off while the two lift engines have corresponding rearward vector to ensure stability. The airframe makes extensive use of composites materials, with some 28 percent by weight constructed of carbon-fibre, primarily in the tail assembly, while the remainder of the structure is mainly aluminum lithium alloys.
The project began in 1975, but was delayed by financial constraints as well as the protracted development of the engine, which meant the prototype did not fly until March 1989. This development program was cancelled due to termination of Defence Ministry funding. Yakolev OKB continued development in refined land-based and naval combat aircraft forms. Four prototypes were built, two continuing in flight testing until 1995, with the other two used for engine and structural testing. To facilitate sales of the Yak-141, Yeltsin has issued decrees allowing tri- or quadripartite agreements with a number of interested organizations in Latin America and Asia.
AC's Specifications
Country of Origin Russia
Builder Yakovlev
Role: air defence
Span 33ft 1 1/2in (10.105m); folded, 19ft 4 1/4in(5.9m)
wing area 341.56ft(2) (31.7m(2))
length overall 60ft 2 3/4in (18.36m)
height 16ft 4 1/4in (5m)
wheel track 9ft lOin (3m)
wheel base 22ft 9 1/4in (6.945m)
tailplane span 19ft 4 1/4in (5.9m)
Weights 25,684lb (11,650kg) Empty, equipped 34,833lb (15,800kg) VTO max take-off weight 42,990lb (19,500kg) STO max take-off weight
Loads 2,204lb (1,OOOkg) VTO max external load 5,732lb (2,600kg) STO max external load 3,858lb (1,750kg) max external fuel
Armament
- 30 mm cannon
- AA-10 Alamo radar-guided medium-range AAM
- AA-11 Archer shortrange IR-guided missile
- bombs
- unguided rockets
limiting load factor 50% fuel, 7g.
Accommodation Single pilot in a Zvezda K36V rocket-boosted zero-zero ejection-seat.
Power Plant
- One Kobchenko/Soyuz R-79-300 vectored-thrust lift/cruise turbofan developing 34,170lb (15,500kg) with afterburning for conventional take-off, or 23,148.5lb (10,500kg) dry, plus
- two Rybinsk RD- 41 turbofan lift engines each rated at a maximum 9,039lb (4,100kg)
Max internal fuel capacity 9,700lb (4,400kg)
Maximum Speed 675 kts (1,250km/hr) Max level speed, sea level
971 kts (1,800km/hr) at 36,089ft (11,OOOm) M=1.8 max achievable Mach numbe
vertical climb rate 49,213ft/min (250m/sec)
service ceilingover 49,000ft (15,000m+)
combat radius
- 351nm (650km) VTO range at sea level, no external weapons
- 372nm (690km) with 4,409lb (2,000kg) weapon load and take-off run of 394ft (120m)
- 755nm (1,400km) at 32,808-39,370ft (10-12,000m)
- 1,133nm (2,100km) max range, with external fuel and short take-off
- 755nm (1,400km) with vertical takeoff and internal fuel
JSF
http://www.globalsecurity.org/military/systems/aircraft/jsf-specs.htm
Function strike fighter
Contractor Lockheed-Martin (Boeing lost the contract)
Service U.S. Air Force U.S. Marine Corps U.K. Royal Navy U.S. Navy
Variants
Conventional Takeoff and Landing (CTOL) Unit Cost $28M
Short Takeoff and Vertical Landing (STOVL) Unit Cost $35M
Carrier-based (CV) Unit Cost $38M
Inventory Objectives U.S. Air Force 2,036 aircraft U.S. Marine Corps 642 aircraft U.K. Royal Navy 60 aircraft U.S. Navy 300 aircraft
Inventory Objectives 1,763 aircraft 609 aircraft 480 aircraft
Propulsion Baseline: P&W F119-PW-100 derivative from F-22r
Alternate Engine: General Electric F120 core Thrust
Empty Weight ~22,500 lbs(USAF) ~24,000 lbs U.S. Navy
Internal Fuel 15,000 lbs(USAF) 16,000 lbs U.S. Navy
Payload 13,000 lbs(USAF) 17,000 lbs ( U.S. Navy)
Maximum Takeoff Weight ~50,000 lbs
Length 45 feet
Wingspan 36 feet(USAF) 30 feet Height( U.S. Navy)
Ceiling ?
Speed supersonic USAF
Combat Radius over 600 nautical miles (USAF)
Crew oneUSAF
Armament ?
First flight 1999 USAF
Date Deployed 2008 USAF
Varients of JSF-35.jpg
This piece of information is quite old and was modified a bit.