Northrop F-5A Freedomfighter The F-5 is a supersonic fighter combining low cost, ease of maintenance, and great versatility. More than 2,000 F-5 aircraft have been procured by the USAF for use by allied nations. The F-5, which resembles the USAF Northrop T-38 trainer, is suitable for various types of ground-support and aerial intercept missions, including those which would have to be conducted from sod fields in combat areas. The F-5 first flew on July 30, 1959 and deliveries to the Tactical Air Command for instructing foreign pilots began in April 1964. Pilots from Iran and South Korea were the first to be trained in the F-5, followed by pilots from Norway, Greece, Taiwan, Spain, and other Free World nations which have adopted the F-5. A two place combat trainer version, the F-5B, first flew in February 1964. In 1966-67, a USAF squadron of F-5s flew combat missions in Southeast Asia for operational evaluation purposes. Engines: 2 * 1800 kg G.E. J85-GE-13 Wing Area: 15.79 m2 Wing Span: 7.70 m Length: 14.38 m Height: 4.01 m Empty Weight: 3667 kg Max.Weight: 3667 kg Take-off Weight: 5206 kg Max. Speed: 1490 km/h Range: 2600 km Ceiling: 15200 m Armament: 2*g20mm Unit cost: 5 million USD

Bell UH-1H Iroquois The Bell UH-1 Iroquois, commonly known as the "Huey," was a multipurpose utility helicopter famous for its use during the Vietnam War. Bell developed the powerful helicopter in the 1950s and produced more than 16,000 between 1955 and 1976, over 7,000 of which served in Vietnam. During service in the Vietnam War, the UH-1 was used for various purposes and various terms for each task abounded. UH-1s tasked with a ground attack or armed escort role were outfitted with rocket launchers, grenade launchers, and machine guns. As early as 1962, UH-1s were modified locally by the companies themselves, who fabricated their own mounting systems.These gunship UH-1s were commonly referred to as Frogs or Hogs if they carried rockets, and Cobras or simply Guns if they had guns.UH-1s tasked and configured for troop transport were often called Slicks due to an absence of weapons pods. Slicks did have door gunners, but were generally employed in the troop transport and medevac roles. UH-1H Iroquois (Huey) Length: 17.398m Height: 4.39522m Rotor Diameter: 14.6304m Empty Weight: 2365.52kg Gross Weight: 4100.54kg Maximum Speed: 217 km/h Cruise Speed: 201.125km/h Power Plant: Lycoming T53-L-13 engine Range: 506.835km

Boeing CH-47 Chinook The Boeing CH-47 Chinook is an American twin-engine, tandem rotor heavy-lift helicopter. Its name is from the Chinook people. Chinooks first were used in combat in 1965 during the Vietnam conflict. By 1968, the Chinook had put in 161,000 hours of flying time, carrying 22.4 million passengers and more than 1.3 million tons of cargo. During the last days of the war, one Chinook is reported to have carried 147 refugees in a single lift. CH-47A, B and C models served with distinction for a decade until the war's end in 1975. Length: Fuselage - 15.9 m. Rotors – 30.18 m Width: 3,78 m and 4.8 m Rotor Diameter: 18.29 m Height: 5.77 m Propulsion: 2 Honeywell 55-GA-714A engines, 4,733 shp (3,529 kW) each Speed: 287 km/h Fuel: 4,043 L Useful Load: 11, 3650 kg Mission Radius: F – 200 nm (370.4 km) G/SD - 400 nm (740.8 km) Max Gross Weight: F - 50,000 lbs. (22,730 kg) G - 54,000 lbs. (24,493 kg)

Cessna 185 - Skywagon The Cessna 185, also known as the Skywagon, is a six-seat, single-engined, general aviation light aircraft manufactured by Cessna. It first flew as a prototype in July 1960, with the first production model being completed in March 1961. The Cessna 185 is a high-winged aircraft with non-retractable conventional landing gear and a tailwheel. Over 4,400 were built with production ceasing in 1985. When Cessna re-introduced some of its most popular models in the 1990s, the tailwheel equipped Cessna 180 and 185 were left to the history books and not resurrected. General characteristics Crew: one Capacity: five passengers Length: 25 ft 9 in (7.85 m) Wingspan: 35 ft 10 in (10.92 m) Height: 7 ft 9 in (2.36 m) Wing area: 174 sq ft (16.2 m2) Empty weight: 1,700 lb (771 kg) Gross weight: 2,800 lb (1,270 kg) Powerplant: 1 × Continental O-470-U , 230 hp (170 kW) Propellers: 2-bladed constant speed, 6 ft 10 in (2.08 m) diameter Performance Maximum speed: 148 kn (170 mph; 274 km/h) Cruise speed: 142 kn (163 mph; 263 km/h) Stall speed: 48 kn (55 mph; 89 km/h) Range: 890 nmi (1,024 mi; 1,648 km) Service ceiling: 17,700 ft (5,400 m) Rate of climb: 1,100 ft/min (5.6 m/s)

Cessna A-37 Dragonfly The Cessna A-37 Dragonfly, or Super Tweet, is light attack aircraft developed from the T-37 Tweet basic trainer in the 1960s and 1970s. The A-37 was introduced during the Vietnam War and remained in peacetime service afterwards. In August 1967, 25 A-37As were sent to Vietnam under the "Combat Dragon" evaluation program, and flew from Bien Hoa Air Base on USAF "air commando" missions, including close air support, helicopter escort, FAC, and night interdiction. Combat loads included high-explosive bombs, cluster munition dispensers, unguided rocket packs, napalm tanks, and the SUU-11/A Minigun pod. For most missions, the aircraft also carried two additional external fuel tanks on the inner stores pylons. During this period the A-37As flew thousands of sorties. None were lost to enemy fire, although two were wrecked in landing accidents. The A-37A was formally named the "Dragonfly", but most pilots called it the "Super Tweet." The Combat Dragon program was successful, but unsurprisingly the combat evaluation revealed some of the deficiencies of the A-37A. The most noticeable problem was that the aircraft lacked range and endurance. Other concerns were heavy control response during attack runs (the flight controls were not power-boosted) and the vulnerability of the aircraft's non-redundant flight control system. General characteristics Crew: 2 Length: 28 ft 3.4 in (8.62 m) Wingspan: 35 ft 10.3 in (10.93 m (including tip tanks)) Height: 8 ft 10.3 in (2.70 m) Wing area: 183.9 ft² (17.09 m²) Empty weight: 6,211 lb (2,817 kg) Max. takeoff weight: 14,000 lb (6,350 kg) Powerplant: 2 × General Electric J85-GE-17A turbojet, 2,850 lbf (12.7 kN) each Performance Maximum speed: 507 mph (440 knots, 816 km/h) at 16,000 ft Cruise speed: 489 mph (425 knots, 787 km/h) at 25,000 ft Range: 800 nm (920 mi, 1,480 km)[citation needed] Combat radius: 400 nm (460 mi, 740 km) with 4,100 lb warload Service ceiling: 41,765 ft (12,730 m) Rate of climb: 6,990 ft/min (35.5 m/s) Armament Guns: 1× .308 in (7.62 mm) GAU-2B/A minigun (mounted in nose) Hardpoints: 8 under-wing with a capacity of 1,230 kg Gun pods: SUU-11/A (1× 7.62 mm M134 minigun), GPU-2/A (1× 20 mm M197 cannon), 30 mm DEFA cannon Rockets: four pods, each with seven 70 mm/2.75 inch rockets (Mk 4/Mk 40 FFAR rockets in a LAU-32/A, LAU-59, or LAU-68 launcher) or (Mk 66/WAFAR rockets in a LAU-131 launcher) Missiles: AIM-9 Sidewinder Bombs: 500 lb (241 kg) Mk.82 (×4 on multiple ejector racks), SUU-14 bomblet dispenser Other: Napalm tanks, SUU-25/A Flare Dispenser