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List Of McDonnell Douglas F-4 Phantom II Variants
The McDonnell Douglas F-4 Phantom II variants were numerous versions and designations of the F-4 and are described below. Production numbers for major versions asterisk indicates converted from other version Variants ;XF4H-1 :Two prototypes for the United States Navy, first flown 1958. ;F4H-1F (F-4A) :Two-seat all-weather carrier-based fighter for the US Navy, J79-GE-2 and -2A engines with 16,100 lbf (71.6 kN) of afterburner thrust each. Named Phantom II in 1959 and redesignated F-4A in 1962; 45 built.Francillon 1979, p.559. ;TF-4A :A small number of F-4As converted into two-seat training aircraft. ;F4H-1 (F-4B) :Two-seat all-weather carrier-based fighter and ground-attack aircraft for the US Navy and Marine Corps. J79-GE-8A or -8B engines with 16,950 lbf (75.4 kN) of afterburner thrust each. Redesignated F-4B in 1962; 649 built.Francillon 1979, pp.559-560. ;DF-4B :F-4Bs converted into drone control aircraft. ;EF-4B :One F-4B converted into an ECM training aircraft. ;NF-4 ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
USAF McDonnell Douglas QF-4E Phantom II
The United States Air Force (USAF) is the air service branch of the United States Armed Forces, and is one of the eight uniformed services of the United States. Originally created on 1 August 1907, as a part of the United States Army Signal Corps, the USAF was established as a separate branch of the United States Armed Forces in 1947 with the enactment of the National Security Act of 1947. It is the second youngest branch of the United States Armed Forces and the fourth in order of precedence. The United States Air Force articulates its core missions as air supremacy, global integrated intelligence, surveillance and reconnaissance, rapid global mobility, global strike, and command and control. The United States Air Force is a military service branch organized within the Department of the Air Force, one of the three military departments of the Department of Defense. The Air Force through the Department of the Air Force is headed by the civilian Secretary of the Air Force, ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
Boom Refueling
Aerial refueling, also referred to as air refueling, in-flight refueling (IFR), air-to-air refueling (AAR), and tanking, is the process of transferring aviation fuel from one aircraft (the tanker) to another (the receiver) while both aircraft are in flight. The two main refueling systems are ''probe-and-drogue'', which is simpler to adapt to existing aircraft, and the ''flying boom'', which offers faster fuel transfer, but requires a dedicated boom operator station. The procedure allows the receiving aircraft to remain airborne longer, extending its range or loiter time. A series of air refuelings can give range limited only by crew fatigue/physical needs and engineering factors such as engine oil consumption. As the receiver aircraft can be topped up with extra fuel in the air, air refueling can allow a takeoff with a greater payload which could be weapons, cargo, or personnel: the maximum takeoff weight is maintained by carrying less fuel and topping up once airborne. Aeri ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
RF-4C Kentucky ANG Landing In Germany 1983
The McDonnell Douglas F-4 Phantom II variants were numerous versions and designations of the F-4 and are described below. Production numbers for major versions asterisk indicates converted from other version Variants ;XF4H-1 :Two prototypes for the United States Navy, first flown 1958. ;F4H-1F (F-4A) :Two-seat all-weather carrier-based fighter for the US Navy, J79-GE-2 and -2A engines with 16,100 lbf (71.6 kN) of afterburner thrust each. Named Phantom II in 1959 and redesignated F-4A in 1962; 45 built.Francillon 1979, p.559. ;TF-4A :A small number of F-4As converted into two-seat training aircraft. ;F4H-1 (F-4B) :Two-seat all-weather carrier-based fighter and ground-attack aircraft for the US Navy and Marine Corps. J79-GE-8A or -8B engines with 16,950 lbf (75.4 kN) of afterburner thrust each. Redesignated F-4B in 1962; 649 built.Francillon 1979, pp.559-560. ;DF-4B :F-4Bs converted into drone control aircraft. ;EF-4B :One F-4B converted into an ECM training aircraft. ;NF-4 ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
AGM-78 Standard ARM
The AGM-78 Standard ARM was an anti-radiation missile developed by General Dynamics, United States. It was built on the airframe of the RIM-66 Standard surface-to-air missile, resulting in a very large weapon with considerable range, allowing it to attack targets as much as away. Overview Originally developed for the US Navy during the late 1960s, the AGM-78 was created in large part because of the limitations of the AGM-45 Shrike, which suffered from a small warhead, limited range and a poor guidance system. General Dynamics was asked to create an air-launched ARM by modifying the RIM-66 SM-1 surface-to-air missile. This use of an "off the shelf" design greatly reduced development costs, and trials of the new weapon began in 1967 after only a year of development. The first operational missiles were issued in early 1968. The AGM-78 was nicknamed the "Starm", an abbreviation of Standard ARM. The first version of the missile, the A1 Mod 0, was little more than an air-launched RIM ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
AGM-45 Shrike
AGM-45 Shrike is an American anti-radiation missile designed to home in on hostile anti-aircraft radar. The Shrike was developed by the Naval Weapons Center at China Lake in 1963 by mating a seeker head to the rocket body of an AIM-7 Sparrow. It was phased out by U.S. in 1992 and at an unknown time by the Israeli Air Force (the only other major user), and has been superseded by the AGM-88 HARM missile. The Israel Defense Forces developed a version of the Shrike that could be ground-launched with a booster rocket, and mounted it on an M4 Sherman chassis as the Kilshon (Hebrew for ''Trident''). History The Shrike was first employed during the Vietnam War by the Navy in 1965 using A-4 aircraft. The Air Force adopted the weapon the following year using F-105F and G Thunderchief Wild Weasel SEAD aircraft, and later the F-4 Phantom II in the same role. The range was nominally shorter than the SA-2 Guideline missiles that the system was used against, although it was a great imp ... [...More Info...] [...Related Items...] OR: [Wikipedia] [Google] [Baidu] |
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