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SKY PILOT by THE ANIMALS

SNOOPY vs THE RED BARON by THE  Royal Guardsmen

 

F-4 PHANTOM

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Aircraft: McDonnell F-4C
Year: 1963
Type: fighter-bomber
Manufacturer: McDonnell Aircraft Corp.
Engine: 2 x General Electric J79GE-15
Power: 17,000 lb (7,711 kg)
Wingspan: 38ft 5in (11.70m)
Length: 58ft 3 3/4in (17.78m)
Height: 16ft 3in (4.95m)
Wing area: 530sq ft (49.23mē)
Max take-off weight: 51,441 lb (23,334 kg)
Empty weight: 28,496 lb (12,926 kg)
Max speed: 1,433mph at 40,000ft (2,306km/h at 12,192m)
Service ceiling: 56,100ft (17,099m)
Range: 538mi (866km)
Crew: 2
Load-armament: 4 missiles; 16,000 lb (7,

 

CLICK IMAGE

 

A-4 SKYHAWK

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Country of Origin:  U.S.A.
B/N or Serial Number: 151194 
Type:  Carrier borne light attack bomber 
Accommodation:  Pilot seated on a Douglas Escapac 1-G3 lightweight ejector seat 
Armament (fixed): Two Mk 12 2Omm cannon with 200 rounds per gun in the wing roots 
Armament (disposable): This is carried on one under fuselage hard point, rated at 1,588kg (3,5001b), and on four under wing hard points, the inner pair each rated at 1,021kg (2,250lb) and the outer pair each at 454kg (1,000lb); a great variety of weapon loads can be carried, including nuclear bombs, the Mk 84 907kg (2,000lb) bomb, the Mk 83 454kg (1,000lb) free-fall or retarded bomb, the Mk 82 227kg (500lb) free-fall or retarded bomb, the Mk 8111 3kg (250lb) free-fall or retarded bomb, the LAU-3/A launcher with 19 69.85mm (2.75in) rockets, the LAU-10/A launcher with four 127mm (Sin) rockets
Electronics and operational equipment: Communication and navigation equipment, plus Bendix automatic flight control, Marconi AN/AVQ-24 head-up display, Texas Instruments AN/AJB-3 bombing system, ANIASN-41 navigation computer, AN/APN153(V) radar navigation, and electronic countermeasures 
Powerplant and fuel system: One 5,080kg (11,200lb) Pratt & Whitney J52-P-408 turbojet 
Performance: Maximum speed 646km/h (1,040mph) with 1,814kg (4,000lb) bomb load; initial climb rate 3,140m (10,300ft) per minute; range 3,220km (2,000 miles) with maximum fuel
Weights: Empty 4,899kg (10,800lb); maximum takeoff 11,113kg (24,500lb) 
Dimensions:  Span 8.38m (27ft,6in); length 12.29m (40ft 4in) excluding probe; height 4.57m (15ft,1Oin); wing area 24.16 square meter (26Osqft) 

 

AC-47D PUFF THE MAGIC DRAGON

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In the early 1960s, Air Force Systems Command began experimenting with side-firing weapons systems for possible use in Vietnam in point defense and night Close Air Support (CAS) roles. In late 1964, the first gunship conversion of a World War II cargo plane was done. The gunship version of the C-47D was initially designated FC-47D (Fighter-Cargo), but was changed to AC (Attack Cargo) primarily because of complaints by traditional fighter pilots. The aircraft had several nicknames: "Spooky", Puff the Magic Dragon", and "Puff".

The AC-47D(S/N 43-48579) was equipped with three SUU-11A 7.62 mm "miniguns" with a 6,000 round per minute rate of fire. The miniguns were mounted in the aft left fuselage, one gun was installed in the aft passenger door area. The other two guns were mounted just forward of the passenger door with the gun barrels pointed out window ports. The AC-47D carried about 16,500 rounds of ammunition on a typical mission.

For night missions, the aircraft carried approximately 48 MK-24 flares. Each flare would last up to three minutes (Mod 3 version) and produced a light of 2 million candlepower. The delivery system was extremely simple, the loadmaster armed and dropped the flare out the cargo door when the pilot signaled by flashing a cargo compartment light.

AC-47 Operations Bulletin #56 - 13 Feb 67 (PACAF)
As employed in Southeast Asia, the flight crew consisted of seven USAF personnel, as well as a Vietnamese observer assigned to aid in the "delta" missions. The aircraft commander (pilot) fired the gun while the copilot performs the normal piloting duties and coordinated the activities of the crew. In the target area the navigator and Vietnamese Air Force observer (8th crewman if assigned) collaborate to accurately pinpoint objectives and coordinate with the ground forces. Two gunners accomplish the preflight, gun loading and in-flight troubleshooting of the SUU-11 guns. The loadmaster arms and manually drops the flares from the rear entrance door upon a light signal from the aircraft commander. A flight mechanic rounds out the crew and is responsible for aircraft systems operation.

    The basic missions on which the AC-47 was employed were:
  1. Defense of ground positions (friendly forts and outposts).
  2. Escort and patrol.
  3. Pre-planned strikes against suitable targets.
  4. Forward air controlling for fighter strikes.

Initial attack procedures began with the aircraft in straight and level flight, and the target just outside and forward of the left prop dome. Usual altitude is between 2500-3000 feet above ground level (AGL); however, this could be adjusted to allow for such variables as weather, ground fire and target identification difficulties. As the target passed under the engine cowling, the aircraft was rolled into a level 30° bank turn. When the (gun site) pipper came on target, firing was commenced in bursts of 3-7 seconds, as required. When the pipper moved off the target to the rear, the firing was ceased and a slight turn was made away from the target for repositioning and subsequent firing passes. If the pipper moved off the target to the front, the degree of bank was increased to realign on target. Airspeed during the maneuver was normally 120 knots indicated air speed (KIAS). Each minigun fired at a rate of 6000 rounds per minute. This provided a coverage over an elliptical area approximately 52 yards in diameter, placing a projectile within every 2.4 yards during a 3 second burst.

The guns were configured for a 12° declination to allow shallower bank angles and more precise aircraft control.

SPECIFICATIONS
Span: 95 ft. 0 in.
Length: 64 ft. 5 in.
Height: 16 ft. 11 in.
Weight: 33,000 lbs. loaded
Armament: Three SUU-11A 7.62 mm "miniguns" firing at up to 6,000 rounds per minute. The AC-47D typically carried about 16,500 rounds of ammunition. Note: Three aircraft initially equipped with 8 or 10 .30-cal. machine guns and others had just two SUU-11A miniguns (due to lack of availability from the manufacturer). Later, the SUU-11A's were replaced by specially designed General Electric MXU-470/A 7.62 mm miniguns. 48 MK-24 Mod 3 flares with 2 million candlepower and a 3 minute maximum burn duration. Note: Initially (in 1964 and early 1965) 30 MK-6 flares of 750,000 candlepower were carried before the MK-24 flares were available. Later in the war, several replacements for the MK-24 flares were proposed including the MK-33 one million candlepower rocket and MLU-32/B99 "Briteye" 5 million candlepower flare.
Engines: Two Pratt & Whitney R-1830s of 1,200 hp. ea.
Crew: Seven or Eight (Pilot, Copilot, Navigator, Flight Engineer, Loadmaster, 2 gunners and a South Vietnamese observer)

PERFORMANCE (C-47D)
Maximum speed: 232 mph.
Cruising speed: 175 mph.
Range: 1,513 miles

OV-10A BRONCO

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The OV-10 Bronco, a rugged, maneuverable, twin-turboprop, multimission aircraft, served with the U.S. Air Force and Marine Corps (OV-10A). The US Navy also used the OV-10. The Navy squadron VAL-4 "Black Ponies" flew them with much success in Vietnam. Internationally the OV-10 served with the military services of West Germany (OV-10B), Thailand (OV-10C), Venezuela (OV-10E), and Indonesia (OV-10F). Designed and built by North American at Columbus, Ohio, the Bronco complemented the performance requirements between jets and helicopters. Faster and more tactically versatile than helicopters, yet slower

 

B-52 STRATO-FORTRESS

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The B-52 D/F long range bombers  were designed to carry nuclear weapons but some were reconfigured and used in the VIETNAM war to drop "Iron Bombs". Their normal bomb load was 84 bombs internally and 24 bombs under the wings. Each bomb weighed 500 pounds. (Sometimes they carried 750 lb bombs.) That's 54,000 pounds of HE, a lot of bang from each aircraft.

Crews and aircraft from the 22nd, 91st, 99th, 306th, 454th, and 461st Bomb Wings rotated through the bombing campaign. Flying out of Andersen Air Force Base on Guam Island (and later U-Tapao Base in Thailand) they had sufficient range to drop their loads on VIETNAM and return without stopping. However to increase their bomb load they normally took off with less than full fuel tanks and refueled in mid-air west of Luzon.

These aircraft worked in threes (called cells) and their attacks were called "Arc Lights". The bombs punched 50 ft holes in the ground and cleared away a lot of jungle. They did not, however, kill great numbers of NVA. Often warned by Russian "Trawlers" sailing near Guam and using state of the art radio intercept equipment, the NVA forces frequently moved out of the target area shortly before the bombs arrived.

Mission

Air Combat Command's B-52 is a long-range, heavy bomber that can perform a variety of missions. The bomber is capable of flying at high subsonic speeds at altitudes up to 50,000 feet (15,166.6 meters). It can carry nuclear or precision guided conventional ordnance with worldwide precision navigation capability.

Features

In a conventional conflict, the B-52 can perform strategic attack, air interdiction, offensive counter-air and maritime operations. During Desert Storm, B-52s delivered 40 percent of all the weapons dropped by coalition forces. It is highly effective when used for ocean surveillance, and can assist the U.S. Navy in anti-ship and mine-laying operations. Two B-52s, in two hours, can monitor 140,000 square miles (364,000 square kilometers) of ocean surface.

All B-52s are equipped with an electro-optical viewing system that uses platinum silicide forward-looking infrared and high resolution low-light-level television sensors to augment targeting, battle assessment, and flight safety, thus further improving its combat ability and low-level flight capability.

Pilots wear night vision goggles (NVGs) to enhance their vision during night operations. Night vision goggles provide greater safety during night operations by increasing the pilot's ability to visually clear terrain, avoid enemy radar and see other aircraft in a covert/lights-out environment.

Starting in 1989, on-going modifications incorporates the global positioning system, heavy stores adapter beams for carrying 2,000 pound munitions, and a full array of advance weapons currently under development.

The use of aerial refueling gives the B-52 a range limited only by crew endurance. It has an un-refueled combat range in excess of 8,800 miles (14,080 kilometers).

The aircraft's flexibility was evident in Operation Desert Storm and again during Operations Allied Force. B-52s struck wide-area troop concentrations, fixed installations and bunkers, and decimated the morale of Iraq's Republican Guard. The Gulf War involved the longest strike mission in the history of aerial warfare when B-52s took off from Barksdale Air Force Base, La., launched conventional air launched cruise missiles and returned to Barksdale -- a 35-hour, non-stop combat mission. During Operation Allied Force, B-52s opened the conflict with conventional cruise missile attacks and then transitioned to delivering general purpose bombs and cluster bomb units on Serbian army positions and staging areas.

Background

For more than 40 years B-52 Stratofortresses have been the backbone of the manned strategic bomber force for the United States. The B-52 is capable of dropping or launching the widest array of weapons in the U.S. inventory. This includes gravity bombs, cluster bombs, precision guided missiles and joint direct attack munitions. Updated with modern technology the B-52 will be capable of delivering the full complement of joint developed weapons and will continue into the 21st century as an important element of our nation's defenses. Current engineering analyses show the B-52's life span to extend beyond the year 2045.

The B-52A first flew in 1954, and the B model entered service in 1955. A total of 744 B-52s were built with the last, a B-52H, delivered in October 1962. Only the H model is still in the Air Force inventory and is assigned to Air Combat Command and the Air Force Reserves.

The first of 102 B-52H's was delivered to Strategic Air Command in May 1961. The H model can carry up to 20 air launched cruise missiles. In addition, it can carry the conventional cruise missile that was launched in several contingencies during the 1990s, starting with Operation Desert Storm and culminating with Operation Allied Force.

General Characteristics

Primary Function: Heavy bomber
Contractor: Boeing Military Airplane Co.
Power plant: Eight Pratt & Whitney engines TF33-P-3/103 turbofan
Thrust: Each engine up to 17,000 pounds
Length: 159 feet, 4 inches (48.5 meters)
Height: 40 feet, 8 inches (12.4 meters)
Wingspan: 185 feet (56.4 meters)
Speed: 650 miles per hour (Mach 0.86)
Ceiling: 50,000 feet (15,151.5 meters)
Weight: Approximately 185,000 pounds empty (83,250 kilograms)
Maximum Takeoff Weight: 488,000 pounds (219,600 kilograms)
Range: Un-refueled 8,800 miles (7,652 nautical miles)
Armament: Approximately 70,000 pounds (31,500 kilograms) mixed ordnance -- bombs, mines and missiles. (Modified to carry air-launched cruise missiles, Harpoon anti-ship and Have Nap missiles.)
Crew: Five (aircraft commander, pilot, radar navigator, navigator and electronic warfare officer)
Accommodations: Six ejection seats
Unit Cost: $53.4 million (fiscal 98 constant dollars)
Date Deployed: February 1955