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
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
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:
Defense of ground positions (friendly forts and outposts).
Escort and patrol.
Pre-planned strikes against suitable targets.
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
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
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