Grumman F- 1. 4 Tomcat - Wikipedia. The Grumman F- 1. The Grumman F-14 Tomcat is an American supersonic, twin-engine, two-seater, variable-sweep wing fighter aircraft. The Tomcat was developed for the United States Navy. Advancements during the Cold War in Soviet long range patrol and bomber aircraft dictated a requirement for a fleet defense fighter that. Project Cars for sale, classic car restorations or street rod restorations. The Boutique Online Store from Singapore for Female Apparels. Affordable Luxury concept. Dresses, tops, rompers, jumpsuit. Tomcat is an American supersonic, twin- engine, two- seater, variable- sweep wingfighter aircraft. The Tomcat was developed for the United States Navy's Naval Fighter Experimental (VFX) program after the collapse of the F- 1. Scroll down the menu and click on highlights to view descriptions and pictures of Drag Racing Vehicles for sale. Hobby Master Collector.com is dedicated to the promotion of the top rated award winning die-cast models produced by Hobby Master and SkyMax. You'll find news, reviews. El Grumman F-14 Tomcat es un caza supers Usn, navy, coast guard, USCG, United states navy, fleet, squadron, wing, flight, helicopter, aircraft, base, naval air base, naval air facility, top gun, f-14 tomcat. B project. The F- 1. American teen- series fighters, which were designed incorporating air combat experience against Mi. G fighters during the Vietnam War. The F- 1. 4 first flew in December 1. U. S. Navy aboard USS Enterprise (CVN- 6. Mc. Donnell Douglas F- 4 Phantom II. The F- 1. 4 served as the U. S. Navy's primary maritime air superiority fighter, fleet defense interceptor and tactical aerial reconnaissance platform. In the 1. 99. 0s, it added the Low Altitude Navigation and Targeting Infrared for Night (LANTIRN) pod system and began performing precision ground- attack missions. Iranian F- 1. 4s reportedly shot down at least 1. Iraqi aircraft during the war, while only 1. Tomcats were lost; at least half of these losses were due to accidents. Navy's active fleet on 2. September 2. 00. 6, having been supplanted by the Boeing F/A- 1. E/F Super Hornet. Navy sought a long- range, high- endurance interceptor to defend its carrier battle groups against long- range anti- ship missiles launched from the jet bombers and submarines of the Soviet Union. Navy needed a Fleet Air Defense (FAD) aircraft with a more powerful radar, and longer range missiles than the F- 4 Phantom II to intercept both enemy bombers and missiles. Air Force by Secretary of Defense. Robert Mc. Namara. Navy F- 1. 11. B variant for TFX and would not be resolved to the Navy's satisfaction. The F- 1. 11 manufacturer General Dynamics partnered with Grumman on the Navy F- 1. B. With the F- 1. B program in distress, Grumman began studying improvements and alternatives. In 1. 96. 6, the Navy awarded Grumman a contract to begin studying advanced fighter designs. Grumman narrowed down these designs to its 3. Connolly, Deputy Chief of Naval Operations for Air Warfare, took the developmental F- 1. A variant for a flight and discovered that it had difficulty going supersonic and had poor carrier landing characteristics. He later testified to Congress about his concerns against the official Department of the Navy position and, in May 1. Congress stopped funding for the F- 1. B, allowing the Navy to pursue an answer tailored to its requirements. The Navy studied the need for VFAX, an additional fighter that was more agile than the F- 4 Phantom for air- combat and ground- attack roles. The company continued to refine the design into 1. VFX called for a tandem two- seat, twin- engined air- to- air fighter with a maximum speed of Mach 2. It would also have a built- in M6. Vulcan cannon and a secondary close air support role. Bids were received from General Dynamics, Grumman, Ling- Temco- Vought, Mc. Donnell Douglas and North American Rockwell. Grumman was selected for the contract award in January 1. Much of the testing, including the first of many compressor stalls and multiple ejections, took place over Long Island Sound. In order to save time and forestall interference from Secretary Mc. Namara, the Navy skipped the prototype phase and jumped directly to full- scale development; the Air Force took a similar approach with its F- 1. The United States Marine Corps was initially interested in the F- 1. F- 4 Phantom II replacement; going so far as to send officers to Fighter Squadron One Twenty- Four (VF- 1. The Marine Corps pulled out of any procurement when development of the stores management system for ground attack munitions was not pursued. An air- to- ground capability was not developed until the 1. AIM- 5. 4 Phoenix missile testing from the F- 1. April 1. 97. 2. The longest single Phoenix launch was successful against a target at a range of 1. April 1. 97. 3. Another unusual test was made on 2. November 1. 97. 3, when six missiles were fired within 3. Mach 0. 7. 8 and 2. So the early arrangement of the AIM- 5. A Phoenix active- radar air- to- air missile, the AIM- 7. E- 2 Sparrow Semi- active radar homing air- to- air missile, and the AIM- 9. J Sidewinder heat- seeking air- to- air missile was replaced in the 1. B (1. 98. 3) and C (1. Phoenix, the F (1. M (1. 98. 2), P (1. Sparrows, and with the Sidewinder, L (1. M (1. 98. 2). Within these versions there are several improved batches (for example, Phoenix AIM- 5. C++). Approximately 6. F- 1. 4As and all F- 1. Ds were modified to carry the pod. The TARPS was upgraded with digital camera in 1. The digital camera was further updated beginning in 1. These upgraded Tomcats were redesignated F- 1. A+, which was later changed to F- 1. B in 1. 99. 1. VFAX was revived in the 1. Navy and Marine Corps's fleets of F- 4s, and A- 7s. VFAX was directed to review the fighters in the USAF Light Weight Fighter competition, which led to the development of the F/A- 1. Hornet as roughly a midsize fighter and attack aircraft. In 1. 99. 4, Congress would reject Grumman proposals to the Navy to upgrade the Tomcat beyond the D model (such as the Super Tomcat 2. Quick. Strike version, and the more advanced Attack Super Tomcat 2. Trials with live bombs had been carried out in the 1. F- 1. 4 was cleared to use basic iron bombs in 1. In Operation Desert Storm, most air- to- ground missions were left to A- 7, A- 6 Intruder and F/A- 1. Hornet squadrons, the F- 1. Following Desert Storm, F- 1. As and F- 1. 4Bs underwent upgrades to avionics and cockpit displays to enable the use of precision munitions, enhance defensive systems, and apply structural improvements. The new avionics were comparable with the F- 1. D; upgraded aircraft were designated F- 1. A (Upgrade) and F- 1. B (Upgrade) respectively. However, the upgrades would have taken too long to implement to meet the gap, and were priced in the billions; Congress considered this too expensive for an interim solution. The LANTIRN pod provided the F- 1. FLIR) camera for night operations and a laser target designator to direct laser- guided bombs (LGB). The Tomcat's LANTIRN pod was altered and improved over the baseline configuration, such as a Global Positioning System / Inertial Navigation System (GPS- INS) capability to allow an F- 1. The pod was carried on the right wing glove pylon. Consequently, Martin Marietta specially developed an interface card for LANTIRN. The Radar Intercept Officer (RIO) would receive pod imagery on a 1. Programmable Tactical Information Display (PTID) or another Multi- Function Display in the F- 1. Initially, the hand controller replaced the RIO's TARPS control panel, meaning a Tomcat configured for LANTIRN could not carry TARPS and the reverse, but eventually a workaround was later developed to allow a Tomcat to carry LANTIRN or TARPS as needed. It features variable geometry wings that swing automatically during flight. For high- speed intercept, they are swept back and they swing forward for lower speed flight. The F- 1. 4 is equipped with an internal 2. M6. 1 Vulcan. Gatling cannon mounted on the left side (unlike the Phantom, which was not equipped with an internal gun in the US Navy), and can carry AIM- 5. Phoenix, AIM- 7 Sparrow, and AIM- 9 Sidewinder anti- aircraft missiles. The twin engines are housed in widely spaced nacelles. The flat area of the fuselage between the nacelles is used to contain fuel and avionics systems, such as the wing- sweep mechanism and flight controls, as well as weaponry, since the wings were not used for carrying ordnance. In an emergency, the F- 1. Such an aircraft would typically be diverted from an aircraft carrier to a land base if an incident did occur. The F- 1. 4 has flown and landed safely with an asymmetrical wing- sweep on an aircraft carrier during testing; this capability could be used in emergencies. Much of the structure is made of titanium, including the wing box, wing pivots, and upper and lower wing skins. Ailerons are not fitted, with roll control being provided by wing- mounted spoilers at low speed (which are disabled if the sweep angle exceeds 5. Two triangular shaped retractable surfaces, called glove vanes, were originally mounted in the forward part of the wing glove, and could be automatically extended by the flight control system at high Mach numbers. They were used to generate additional lift (force) ahead of the aircraft's center of gravity, thus helping to compensate for the nose- down pitching tendencies at supersonic speeds. Automatically deployed at above Mach 1. F- 1. 4 to pull 7. Mach 2 and could be manually extended with wings swept full aft. They were later disabled, however, owing to their additional weight and complexity. The bottom surface is split into left and right halves, the tailhook hangs between the two halves, an arrangement sometimes called the . De Laval nozzles were also fitted to the engine's exhaust. John Lehman, Secretary of the Navy in the 1. U. S. Congress that the TF3. F- 1. 4 combination was . A high frequency of turbine blade failures led to the reinforcement of the entire engine bay to limit damage from such failures. The engines also had proved to be extremely prone to compressor stalls, which could easily result in loss of control, severe yaw oscillations, and could lead to an unrecoverable flat spin. At specific altitudes, exhaust produced by missile launches could cause an engine compressor stall. This led to the development of a bleed system that temporarily blocks the frontal intake ramp and reduces engine power during missile launch. With the TF3. 0, the F- 1. F- 1. 5A's ratio of 0. General Electric F1. It comprises a double nosewheel and widely spaced single main wheels. There are no hardpoints on the sweeping parts of the wings, and so all the armament is fitted on the belly between the air intake ramps and on pylons under the wing gloves. Internal fuel capacity is 2,4. US gal (9,1. 00 l): 2. US gal (1,1. 00 l) in each wing, 6. US gal (2,6. 00 l) in a series of tanks aft of the cockpit, and a further 4. US gal (1,7. 30 l) in two feeder tanks. It can carry two 2.
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