Lockheed FA-33 Timber Wolf

Lockheed FA-33 Timber Wolf

Multirole jet fighter

General characteristics
• Crew: 1
• Length: 69 ft 2 in)
• Wingspan: 50 ft 9 in to 54 ft 9 in)
• Height: 15ft
• Wing area: 81.87
• Empty weight: 14,375 kg
• Loaded weight: 20,000 kg
• Max. takeoff weight: 30,000 kg
• Powerplant: 1× G Pratt & Whitney YF220 , 65,000

Performance
•
• * Maximum speed: Mach 6.4
• * Cruise speed: Mach 3.4+ est
• * Combat radius: 600-520 mi
• * Service ceiling: 95,000 ft (28.95600m)
• * Wing loading: 70 lb/ft² (456 kg/m²

Guns: 2 × General Dynamics GAU-22/A Equalizer 25 mm (0.984 in) 4-barreled gatling cannon, internally mounted with 180 rounds[N 12][157]
Hardpoints: 6 × external pylons on wings with a capacity of 15,000 lb (6,800 kg)[157][162] and 2 internal bays with 2 pylons each[162] for a total weapons payload of 18,000 lb (8,100 kg)[124] and provisions to carry combinations of:
Missiles: ** Air-to-air missiles:
AIM-120 AMRAAM
AIM-9X Sidewinder
IRIS-T
MBDA Meteor (Pending further funding)[343]
JDRADM (after 2020)[344]
Air-to-surface missiles:
AGM-154 JSOW
AGM-158 JASSM[163]
Brimstone missile
Joint Air-to-Ground Missile
SOM
Anti-ship missiles:
JSM
Bombs: ***Mark 84, Mark 83 and Mark 82 GP bombs
Mk.20 Rockeye II cluster bomb
Wind Corrected Munitions Dispenser capable
Paveway-series laser-guided bombs
Small Diameter Bomb (SDB)
JDAM-series
B61 nuclear bomb[345]

Avionics

Northrop Grumman Electronic Systems AN/APG-81 AESA radar
Northrop Grumman Electronic Systems AN/AAQ-37 Distributed Aperture System (DAS) missile warning system
BAE Systems AN/ASQ-239 (Barracuda) electronic warfare system
Harris Corporation Multifunction Advanced Data Link (MADL) communication system


AN/APG-81

The AN/APG-81 is an Active Electronically Scanned Array (AESA) designed by Northrop Grumman Electronic Systems for the F-35 Lightning II.
The Joint Strike Fighter AN/APG-81 AESA radar is a result of the US government's competition for the world's largest AESA acquisition contract. Westinghouse Electronic Systems (acquired by Northrop Grumman in 1996) and Hughes Aircraft (acquired by Raytheon in 1997) received contracts for the development of the Multifunction Integrated RF System/Multifunction Array (MIRFS/MFA) in February 1996.[1] Lockheed Martin and Northrop Grumman were selected as the winners of the Joint Strike Fighter competition; The System Development and Demonstration (SDD) contract was announced on 26 October 2001.
The AN/APG-81 is a successor radar to the F-22's AN/APG-77. Over 3,000 AN/APG-81 AESA radars are expected to be ordered for the F-35, with production to run beyond 2035, and including large quantities of international orders. As of August 2007, 8 APG-81s have already been produced and delivered. The first three blocks of radar software have been developed, flight tested, and delivered ahead of schedule by the Northrop Grumman Corporation. Capabilities of the AN/APG-81 include the AN/APG-77's air-to-air modes plus advanced air-to-ground modes including high resolution mapping, multiple ground moving target detection and track, combat identification, electronic warfare, and ultra high bandwidth communications. The current F-22 production radar is the APG-77v1, which draws heavily on APG-81 hardware and software for its advanced air-to-ground capabilities.[2]
In August 2005, the APG-81 radar was flown for the first time aboard Northrop Grumman's BAC 1-11 airborne laboratory. Since then, the radar system has accumulated over 300 flight hours, maturing all five blocks of software. The first radar flight on Lockheed Martin's CATBird avionics test bed aircraft took place in November 2008. Announced on 6/22/10: The radar met and exceeded its performance objectives successfully tracking long-range targets as part of the first mission systems test flights of the F-35 Lightning II BF-4 aircraft.[3]
The AN/APG-81 team won the 2010 David Packard Excellence in Acquisition Award for performance against jammers.

The Lockheed Martin Sniper Advanced Targeting Pod (ATP), designated AN/AAQ-33 in U.S. Military Service, provides positive target identification, autonomous tracking, coordinate generation, and precise weapons guidance from extended standoff ranges. The Sniper ATP is used on the F-15E Strike Eagle, F-16 Fighting Falcon, A-10 Thunderbolt II aircraft, B-1 (Rod Pod), UK Harrier GR9,.[1] and Canadian CF-18 Hornet. [2] The Sniper ATP is in service with Norway, Oman, Poland, Singapore, Canada, Belgium, Turkey, Saudi Arabia[3] and the UK MoD.[4][5] In July 2007, Sniper ATP was acquired by Pakistan, making it the tenth country in the world to be in possession of the Sniper pod.[6] The Sniper ATP contains a laser designator and tracker for guiding laser-guided bombs. The pod also features a third-generation FLIR receiver and a CCD television camera. FLIR allows observation and tracking in low light / no light situations, while the CCD camera allows the same functions during day time operations.
A team of Lockheed Martin UK, BAE Systems and SELEX Galileo (formerly Selex S&AS) has successfully demonstrated and flown a Sniper ATP on board a Tornado GR4 combat aircraft.
The U.S. Air Force initial seven-year contract for Sniper ATP has potential value in excess of $843 million. The Sniper ATP has delivered over 125 pods and the U.S. Air Force plans to procure at least 522 Sniper ATPs.
Panther is the export equivalent to the Lockheed Martin Sniper Extended Range (XR) targeting pod.

Multifunction Advanced Data Link (MADL) is a future data waveform to provide secure data-linking technology between stealth aircraft. It began as a method to coordinate between F-35 aircraft (the Joint Strike Fighter), but HQ Air Combat Command wants to expand the capabiltiy to coordinate future USAF strike forces of all AF stealth aircraft, including the B-2, F-22, and unmanned systems. MADL is expected to provide needed throughput, latency, frequency-hopping and anti-jamming capability with phased Array Antenna Assemblies (AAAs) that send and receive tightly directed radio signals.[1]
The Office of the Undersecretary of Defense for Acquisition, Technology and Logistics directed the Air Force and Navy to integrate MADL among the F-22, F-35 and B-2, to one another and to the rest of network.

The FA-70 need not be physically pointing at its target for weapons to be successful. This is possible because of sensors that can track and target a nearby aircraft from any orientation, provide the information to the pilot through his helmet (and therefore visible no matter which way they are looking), and provide the seeker-head of a missile with sufficient information. Recent missile types provide a much greater ability to pursue a target regardless of the launch orientation, called "High Off-Boresight" capability, although the speed and direction in which the munition is launched must physically speaking nonetheless affect the chance of success. Sensors use combined radio frequency and infra red (SAIRST) to continually track nearby aircraft while the pilot's helmet-mounted display system (HMDS) displays and selects targets. The helmet system replaces the display suite-mounted head-up display used in earlier fighters.
The FA-70's systems provide the edge in the "observe, orient, decide, and act" OODA loop; stealth and advanced sensors aid in observation (while being difficult to observe), automated target tracking helps in orientation, sensor fusion simplifies decision making, and the aircraft's controls allow action against targets without having to look away from them.

The Fly-By-Light Advanced System Hardware (FLASH) program is developing and demonstrating dual use fly-by-light hardware for flight control systems on military and commercial aircraft. Under the transport aircraft portion of this program, we and our industry teammates are demonstrating two representative fly-by-light systems. These fly-by-light demonstrations include a ground demonstration of a partial primary flight control system and a flight demonstration of an aileron trim control system. This paper describes these and discusses the dual use fly-by-light hardware developed for transport aircraft as well as the associated FLASH program demonstrations.

Adaptive Camouflage

Lightweight optoelectronic systems built around advanced image sensors and display panels have been proposed for making selected objects appear nearly transparent and thus effectively invisible. These systems are denoted "adaptive camouflage" because unlike traditional camouflage, they would generate displays that would change in response to changing scenes and lighting conditions. Fa-70 use 3 Generation based off of snake skin design

Next Generation Jammer

The United States Marine Corps is considering replacing their Northrop Grumman EA-6B Prowler electronic attack aircraft with F-35s that have stealthy jammer pods attached.[204] On 30 September 2008, the United States Navy outlined the basic requirements of the NGJ and stated that the design must be modular and openThe Navy has selected four companies to submit designs for the Next Generation Jammer.[206] The NGJ will also have cyber attack capabilities where the AESA radar is used to insert tailored data streams into remote systems. the ITT-Boeing design for the NGJ includes six AESA arrays for all around coverage The team has been awarded a $42 million contract to develop their design based on ITT's experience with broadband electronically steerable antenna arrays.[2At the same time contracts were also awarded to Raytheon, Northrop Grumman and BAE Systems.

Pratt & Whitney YF220pw-200

Scram-LACE

Scramjet

are mechanically very similar to ramjets. Like a ramjet, they consist of an inlet, a combustor, and a nozzle. The primary difference between ramjets and scramjets is that scramjets do not slow the oncoming airflow to subsonic speeds for combustion, they use supersonic combustion instead. The name "scramjet" comes from "supersonic combusting ramjet." Since scramjets use supersonic combustion they can operate at speeds above Mach 6 where traditional ramjets are too inefficient. Another difference between ramjets and scramjets comes from how each type of engine compresses the oncoming air flow: while the inlet provides most of the compression for ramjets, the high speeds at which scramjets operate allow them to take advantage of the compression generated by shock waves, primarily oblique shocks.[20]
Very few scramjet engines have ever been built and flown. In May 2010 the Boeing X-51 set the endurance record for the longest scramjet burn at over 200 seconds.[21]

Precooled jets / LACE

Intake air is chilled to very low temperatures at inlet in a heat exchanger before passing through a ramjet and/or turbojet and/or rocket engine. Easily tested on ground. Very high thrust/weight ratios are possible (~14) together with good fuel efficiency over a wide range of airspeeds, Mach 0-5.5+; this combination of efficiencies may permit launching to orbit, single stage, or very rapid, very long distance intercontinental travel. Exists only at the lab prototyping stage. Examples include RB545, Reaction Engines SABRE, ATREX. Requires liquid hydrogen fuel which has very low density and requires heavily insulated tankage.

Thrust Vector Control
Thrust Vector Control or Thrust Vectoring is a technology that deflects the mean flow of an engine jet from the centerline in order to transfer some force to the aimed axis. By that imbalance, a momentum is created and used to control the change of attitude of the aircraft. Among other things, thrust vectoring greatly improves maneuverability, even at high angles of attack or low speeds where conventional aerodynamic control surfaces lose all effectiveness. Thrust Vector Control is currently achieved by complex arrays of mechanical actuators capable of modifying the geometry of the nozzle and thus defect the flow. This variable geometry greatly increases weight and maintenance to the engine, and therefore limits the benefits from vectoring the thrust.