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"The TH-55 Trainer or better known as the TH-55 Osage was two-seater light pilot training helicopter used by the U.S Army. The Trainer was initially designed as a fully-glazed cockpit with seating for two pilots, or a pilot and passenger. It also had an open-framework fuselage and a three-blade articulated rotor. Manufactured by Hughes Helicopters, the TH-55 Trainer first flew in October 1956. It was produced as the Model 269 family of light utility helicopters, some of which were marketed as the Model 300. Also known as the Hughes 269 was created with a fully articulated, counter-clockwise rotating, three-bladed main rotor, and a two-bladed tail rotor that would remain as distinctive characteristics of all its variants. It also has shock absorber-dampened, skid-type landing gear. The flight controls are directly linked to the control surfaces of the helicopter so there is no hydraulics in the 269. There are generally two sets of controls, although this was optional on the civil 269A. The TH-55 Trainer was powered by a Lycoming O-360-C2B four-cylinder horizontally-opposed air-cooled engine providing a top speed of 136 km/h and a flying time of 2.6 hours. "

"The CV-22 Osprey is a joint service, multimission, military tiltrotor aircraft. It combines the vertical takeoff and landing qualities of a helicopter with the long range, fuel efficiency and speed characteristics of a turboprop aircraft. Built by the joint development team of Bell Helicopter Textron and Boeing Helicopters collectively known as Bell Boeing, its primary role is to conduct long range infiltration, exfiltration and resupply missions for special operations forces. The CV-22 is the United States Air Force version of the US Marine Corps MV-22 Osprey. Formally approved for full-rate production by the Pentagon on September 28, 2005, the Osprey is the world's first production tiltrotor aircraft. The CV-22 is versatile and self-deployable, offering increased speed and range over other rotary wing aircraft. It can perform missions that would normally require both fixed wing and rotary wing aircraft. It is equipped with integrated threat countermeasures, a terrain-following radar, a forward-looking infrared sensor, and other advanced avionics systems that allow it to operate at low altitude in adverse weather conditions and medium to high threat environments. The first two test aircraft were delivered to Edwards Air Force Base (AFB), California in September 2000 for flight testing. The first operational CV-22 was delivered to the 58th Special Operations Wing at Kirtland AFB, New Mexico on March 20, 2006, and aircrew training began in August 2006. Initial operating capability of the aircraft is scheduled for 2009, with a total of 50 CV-22s delivered by 2017. "

"The CH-53E Super Sea Stallion is the largest and heaviest helicopter in the history of the United States Military. The CH-53E is commonly referred to as the Hurricane Maker. Built by Sikorsky Aircraft for the United States Marine Corps, the CH-53E served both the Navy and Marines in the heavy lift transport role. The CH-53E Super Sea Stallion is the larger version of the CH-53 Sea Stallion. The CH-53E Stallion was configured with 3 gas turbine engines and in flight refueling. The said aircraft was used to transport personnel and equipment, lift heavy loads and conduct minesweeping missions. In addition to that, the CH-53E is also used for long range delivery and re supply of special operations and combat rescue missions. The CH-53E Super Stallion van transports up to 55 troops and has an external load lift system that allows the helicopter to carry a load up to 16,330 kg. The CH-53E has a speed of 278 km/h and a maximum un-refueled range of 2,000 km. The range and endurance of the CH-53E can be extended by Flight refueling. The general characteristics of the CH-53E are as follows: 2 pilots, 1 right gunner, 1 left gunner, 1 tail gunner, the capacity of the CH-53E aircraft is 37 troops, payload is at 32,000 pounds, length is at 99 ft and ½ inches, rotor diameter is at 79ft, height is at 27ft 9 inches, Disc area is at 4,900 square feet, empty weight is 33,226 pounds, maximum take off weight is 73,500 pounds and the power plant is 3x general electric T64-GE-416A turboshafts, 4,380 shp each. For the performance of the CH-53E Super Stallion, the maximum speed is 170 knots, range is 600 nm, service ceiling is at 18,500 ft, rate of climb is 2,500 ft/min and the armament are guns, chaff and flare dispensers. "

"The Japanese A6M Zero is the most famous Japanese helicopter aircraft from the Second World War. Its code name is Zeke. The Japanese A6M was built as a land-based, carrier borne and a seaplane. The Japanese A6M Zero is indeed an excellent helicopter. The Japanese A6M aircraft was designed by Mitsubishi, it first flew on April 1, 1939. In addition to this, Mitsubishi and Nakajima built 10,937 Japanese A6M Zero helicopters. The Zeros are said to be the best fighters of Japan during WW II. They were the ones who spearheaded the advances from Pearl Harbor to the Battle of Midway, where Japan lost a number of pilots and planes. A combination of admirable maneuverability and very long range made the Japanese A6M Zero one of the supreme fighters of its era. The Japanese A6M Zero is armed with various guns but the common set up is: two 20mm cannons in outer wings and two 12.7 mm guns in the fuselage. The Japanese A6M is very noteworthy for being the first carrier based fighter to outperform its land based equivalents. The Japanese A6M Zero achieved a famous reputation which was a lot better than its contemporaries. The Japanese A6M Zero’s first variant, A6M1, which is powered by a 780-hp, was first flown on April 1, 1939. The second one was the A6M2 which is powered by a 925-hp Nakajima Sakae engine. Other variants are as follows: the A6M2-K which is a two seat trainer, the A6M2-N which is a Nakajima built float plane version, and the A6M5 which is a performance increased version. "

"The Pfalz D.III is a World War I fighter aircraft manufactured by Pfalz Flugzeugwerke Gmbh. In August 1917, deliveries to operational units began. Jasta 10 was the first recipient followed by Jasta 4. The D.III was generally inferior to the Albatros D.III and D.V. due to its heavy controls, lack of speed, lack of power or lack of climb compared to the Albatros. The aircraft also slipped in turns, leading to crashes when unwary pilots turned at very low altitudes. The Pfalz's primary advantage was its strength and sturdiness. However, the Pfalz could safely dive at high speeds due to its twin-spar lower wing, making it well-suited to attack observation balloons which are usually heavily defended with anti-aircraft guns trained to the balloon's altitude. The primary user and operator of the D.III is the German Empire (Luftstreitkrafte). Currently, there are no known D.IIIs which survived, although there are several flying replicas that existed. "

"The Me-109 Messerschmitt was designed by Willy Messerschmitt and was originally powered by a Rolls-Royce Kestrel V engine. It was one of the first true modern fighters of the era. The prototype Me-109 first flew in 1935 and that same year, the Me-109 won a fighter competition. The Me-109B and C models achieved great success in Spain with the Legion Condor's fighter unit. The progressive development in the pre-war years resulted in a more powerful and heavier armed versions of the ME-109. The Me-109 was flown by the three top-scoring fighter aces of World War II including Gunther Rall, with 275 victories. Bf 109 was the official designation, since its design was sent in by the Bayerische Flugzeugwerke company and was used extensively in all official German documents dealing with this aircraft. After July 1938, the company was renamed as Messerschmitt AG, the time when Erhard Milch finally allowed Willy Messerschmitt to acquire the company. The ""Me"" designation and mdash (except those already assigned with the Bf prefix) were to be carried by all Messerchmitt aircraft since then. The Me-109 has basically the smallest airframe that Willy Messerschmitt attached to the most powerful engine. The Me-109 remained a formidable air superiority fighter throughout World War II. "

"Gemini 4 (officially Gemini IV) was a June 1965 manned space flight in NASA's Gemini program. It was the 2nd manned Gemini flight, the 10th manned American flight and the 18th spaceflight of all time (includes X-15 flights over 100 km). It was crewed by James McDivitt and Edward White. Gemini 4 would be the first multi-day space flight by the United States, designed to show that it was possible for humans to remain in space for the length of time required to fly the moon and back. A second objective for the four-day, 62-orbit mission was for Gemini 4 to rendezvous and fly in formation with the spent second stage of its Titan II booster rocket. And although not originally scheduled for this mission, Gemini 4 would also see the first ever American Extra-vehicular activity (EVA, known popularly as a space walk). NASA moved up the original schedule after Aleksei Leonov on Voskhod 2 the previous March performed the first EVA ever, lest the US appear to be falling behind the Soviets in the space race. Gemini 4 would set a record for flight duration, and ease fears about the medical consequences of longer missions. It also would also be the first use of the new Mission Control center outside Houston, which because of the flight's long duration, had to conduct three-shift operations "