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Boeing B-17 Flying Fortress

Boeing B-17 Flying Fortress

The B-17 Flying Fortress is one of the most famous airplanes ever built. The B17 prototype first flew July 28, 1935. Few B-17s were in service on Dec. 7, 1941, but production quickly accelerated. The aircraft served in every World War II combat zone, but is best known for daylight strategic bombing of German industrial targets. Production ended in May 1945, and totaled 12,726.

In response for the Army’s request for a large, multiengine bomber, the B-17 (Model 299) prototype, financed entirely by Boeing, went from design board to flight test in less than 12 months. General features on the B-17 include its mid-wing monoplane design, aluminum-clad exterior, four radial engines, massive wing structure and heavy armament. It was the first Boeing airplane with the distinctive, and enormous, tail for improved control and stability during high-altitude bombing.

Although many U.S. airmen and craft contributed to the Allied victory in World War II, the B-17 has become especially symbolic of the self-reliance, daring and sacrifice of American airmen during the war. American confidence in the B-17 became the cornerstone for the Air Corps doctrine of strategic “daylight” bombing in German-occupied Europe.

The G series could hold a crew of 10, including pilot, co-pilot, bombardier, radio operator, navigator, dorsal turret gunner, two waist gunners, ball turret gunner and tail gunner. Typical for B-17Gs are the four 1,380-horsepower Wright GR1820-97 Cyclone air-cooled, nine-cylinder radial engines equipped with exhaust driven turbochargers.  General features include the raised cockpit section and Plexiglas nose cone. Characteristic of all B-17s, starting with the E series, is the massive dorsal fin, which gracefully sweeps to merge with the fuselage. All B-17s have retractable tail-wheel landing gear. The empty weight of the airplane is 32,720 pounds. Fully armed and loaded, B-17s weigh 65,600 pounds. Payloads of 4,000-5,000 pounds were typical but up to 17,600 pounds could be carried for less than maximum range. The maximum speed was 300 miles per hour at 30,000 feet.

While the B-17s were used in the Pacific, by 1944 the B-29 had replaced the B-17 for use in the Pacific Theater. While in the Pacific, the planes earned a deadly reputation with the Japanese, who dubbed them “four-engine fighters.” The Fortresses were also legendary for their ability to stay in the air after taking brutal poundings. They sometimes limped back to their bases with large chunks of the fuselage shot off. B-17s were initially intended as a fast, land-based bomber, which could patrol at sea and intercept naval vessels.

The B-17 went through several alterations in each of its design stages and variants. By the time the definitive B-17 G appeared, the number of guns had been increased from seven to 13, the designs of the gun stations were finalized, and other adjustments were complete. The B-17 G was the final version of the B-17, incorporating all changes made to its predecessor, the B-17 F, and in total 8,680 was built, the last one on 9 April 1945. Boeing plants built a total of 6,981 B-17s in various models, and another 5,745 were built under a nationwide collaborative effort by Douglas and Lockheed (Vega). Many B-17 Gs were converted for other missions such as cargo hauling, engine testing and reconnaissance. Initially designated SB-17G, a number of B-17Gs were also converted for search-and-rescue duties, later to be re-designated B-17H.

Late in World War II, at least 25 B-17s were fitted with radio controls, loaded with 20,000 pounds (9,000 kg) of high-explosives, dubbed “BQ-7 Aphrodite missiles”, and used against U-boat pens and bomb-resistant fortifications.

Specifications

Wing Span: 103 feet, 10 inches
Length: 74 feet, 4 inches
Height: 19 feet, 1 inches
Weight: 55,000 pounds loaded
Armament: Thirteen .50-caliber machine guns with normal bomb load of 6,000 pounds
Engines: Four Wright “Cyclone” R-1820s of 1,200 horsepower each
Cost: $276,000
Maximum speed: 300 mph.
Cruising speed: 170 mph.
Range: 1,850 miles
Service Ceiling: 35,000 feet
Memphis Bell

McDonnell Douglas F-4 Phantom II

The McDonnell two-place, twin jet, all-weather F-4 Phantom II, with top speeds more than twice that of the speed of sound, was one of the most versatile fighters ever built. A fast and powerful aircraft that proved itself in roles such as interceptor, air-superiority fighter, attack aircraft, and reconnaissance platform. The F-4 was built in large quantities, had a significant combat history, and still remains in service with a number of foreign air arms, over 40 years after its introduction.

The F-4 was put into service by the Air Force and Navy serving a variety of roles in the Vietnam conflict. The final application of the F-4 by the U.S. was in the “Wild Weasel” role for suppressing enemy air defense systems. F-4 production ended in 1979 after over 5,000 had been built-more than 2,600 for the U.S. Air Force, about 1,200 for the U.S. Navy and U.S. Marine Corps, and the rest for friendly foreign nations. Later versions of the aircraft were in the U.S. Air Force inventory until December 1995.

Under its own financing and initiative, McDonnell Aircraft began developing an all-weather attack fighter in August 1953, shortly after it lost a competitive bid to build a Navy supersonic air-superiority fighter. McDonnell had already produced more than 1,000 carrier-based jet aircraft, the FH-1 Phantom, the F2H Banshee and the F3H Demon.

In 1954, the Navy selected McDonnell Aircraft to begin production of the fighter, designated the F4H, which was to be a fleet defense fighter that could take off from an aircraft carrier, have a cruise distance of 250 mi, intercept intruders, and then return to the carrier 3 hr after takeoff. The aircraft was to be armed with missiles and would not carry guns. It would operate as a high-speed (Mach number of 2), standoff missile launcher that would not engage in close-in combat. . Just 31 months after its first flight, the F-4 was the U.S. Navy’s fastest, highest-flying and longest-range fighter. It first flew May 27, 1958, and entered service in 1961. It was named Phantom II on July 3, 1959, during a ceremony held at the McDonnell plant in St. Louis, Mo., to celebrate the company’s 20th anniversary.

During the first few years of the Vietnam conflict, the U.S. found itself engaging enemy aircraft such as the MiG-17 and MiG-19 that were relatively agile and could easily outmaneuver the heavier U.S. aircraft (F-4 and F-105) that had been designed without requirements for close dogfighting or close weapons such as a gun. Initial tactics used by U.S. pilots to try and turn with enemy aircraft had been relatively unsuccessful, and it had become apparent that missiles in use at that time were relatively unreliable at long ranges. Pilot training and revised tactics were ultimately employed to blunt the threat and use U.S. aircraft to an advantage, but the lack of maneuverability and a gun for close-in combat became issues for the Air Force. A new Air Force version known as the F-4E was equipped with a nose mounted M61 cannon, and additional deliveries to the Air Force began in October 1967.

Both U.S. military flight demonstration teams, the Navy Blue Angels and the Air Force Thunderbirds, flew the Phantom II from 1969 to 1973.  The 5,000th Phantom was delivered on May 24, 1978, in ceremonies that also marked the 20th anniversary of the fighter’s first flight, and McDonnell Douglas delivered the last St. Louis-built Phantom II in October 1979.

By 1998, approximately 800 were still in service around the world. With the upgrades already performed and those under contract, the F-4 Phantom II will probably still be flying in 2015 — nearly 60 years after its first flight.

The Navy fighter garnered a host of world speed and time-to-climb records. On 06 December 1959 Commander L.E. Flint, piloting a McDonnell F4H-1 Phantom II powered by two GE J-79 engines bettered the existing world altitude record by reaching 98,560 feet over Edwards Air Force Base.

Specifications
First flight: May 27, 1958 (prototype YF4H-1)
Wingspan: 38 feet 5 inches
Length: 58 feet 3 inches
Height: 16 feet 6 inches
Ceiling: 56,100 feet
Range: 1,750 miles
Weight: 55,597 pounds
Power plant: Two 17,900-pound-thrust General Electric J79-GE-17 jet engines
Speed: 1,485 mph (max.)
Accommodation: Two crew
Armament: 15,983 pounds of weapons, including 20 mm nose-mounted M-61 “Vulcan” cannon

McDonnell Douglas F-4 Phantom II

McDonnell Douglas F-15 Eagle

The F-15 Eagle is probably the most recognizable military jet fighter in the skies today having held the distinction of the premier jet fighter over the past 30 years. The F-15 is the only operational jet fighter to have never been shot down in combat. Along with the US, the air forces of Israel, Saudi Arabi, and Japan have all flown the F-15.

The F-15 was designed to remain highly maneuverable in all weather conditions and to carry a variety of weapons. The F-15′s superior maneuverability and acceleration are achieved through high engine thrust-to-weight ratio and low wing loading. Low wing-loading is a vital factor in maneuverability and, combined with the high thrust-to-weight ratio, enables the aircraft to turn tightly without losing airspeed.

The pilot’s head-up display projects on the windscreen all essential flight information gathered by the integrated avionics system. This display, visible in any light condition, provides information necessary to track and destroy an enemy aircraft without having to look down at cockpit instruments.

The first F-15A flight was made in July 1972, and the first flight of the two-seat F-15B trainer was made in July 1973. The first Eagle F-15B was delivered in November 1974, and in January 1976, the first Eagle destined for a combat squadron was delivered.

The single-seat F-15C and two-seat F-15D models entered the Air Force inventory beginning in 1979.

The F-15E Strike Eagle is a two-seat, dual-role, totally integrated fighter for all-weather, air-to-air and deep interdiction missions, 237 were built between 1985-2001. The rear cockpit is upgraded to include four multi-purpose CRT displays for aircraft systems and weapons management. The digital, triple-redundant Lear Siegler flight control system permits coupled automatic terrain following, enhanced by a ring-laser gyro inertial navigation system.

McDonnell Douglas F-15 Eagle

Specifications
Speed: 1,875 mph
Range: 2,400 miles
Height: 18 feet 8 inches
Length: 63 feet 9 inches
Wingspan: 42 feet, 10 inches
Weight: 68,000 pounds