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The Apollo Gyro AG1 is a Hungarian autogyro produced by Apollo Ultralight Aircraft of Eger and introduced in 2012. The aircraft is supplied ready-to-fly. The aircraft is supplied ready-to-fly. [ 1 ]
This category is for aircraft designed, manufactured or marketed by Apollo Ultralight Aircraft. Pages in category "Apollo Ultralight Aircraft aircraft" The following 6 pages are in this category, out of 6 total.
Apollo Ultralight Aircraft is a Hungarian aircraft manufacturer based in Eger.The company specializes in the design and manufacture of ultralight aircraft, gyroplanes and ultralight trikes, in the form of kits for amateur construction and ready-to-fly aircraft for the European Fédération Aéronautique Internationale microlight and the American light-sport aircraft categories.
AG1 and AG-1 may refer to: Apollo Gyro AG1, a Hungarian autogyro; Christopher AG-1, a proposed Second World War American assault glider; Hispasat AG1, a Spanish ...
The reduction in parts costs is aided by using selective laser melting in the production of some metallic parts. [13] [18] The resulting F-1B engine is intended to produce 1,800,000 lbf (8.0 MN) of thrust at sea level, a 15% increase over the approximate 1,550,000 lbf (6.9 MN) of thrust that the mature Apollo 15 F-1 engines produced.
Apollo computer DSKY user interface unit LM DSKY interface diagram. The user interface to the AGC was the DSKY, standing for display and keyboard and usually pronounced "DIS-kee". It has an array of indicator lights, numeric displays, and a calculator-style keyboard. Commands were entered numerically, as two-digit numbers: Verb and Noun.
On the Apollo 6 uncrewed Block I flight, the SM was painted white to match the command module's appearance. On Apollo 1, Apollo 4, and all the Block II spacecraft, the SM walls were left unpainted except for the EPS and ECS radiators, which were white. The EPS and ECS radiators were redesigned for Block II.
The Orion spacecraft, which was developed to follow the Space Shuttle program, uses a Mercury and Apollo-style escape rocket system, while an alternative system, called the Max Launch Abort System (MLAS), [4] was investigated and would have used existing solid-rocket motors integrated into the bullet-shaped protective launch shroud.