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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.
Engineers at Arnold Air Base with an Apollo service module engine Apollo Service Module Propulsion System The service propulsion system ( SPS ) engine was originally designed to lift the CSM off the surface of the Moon in the direct ascent mission mode, [ 20 ] The engine selected was the AJ10-137 , [ 21 ] which used Aerozine 50 as fuel and ...
Apco System K; Apco Tetra; Apco Tigra ... (Apollo Ultralight Aircraft / Halley Ltd., Eger, Hungary) ... Apollo Delta Jet 2; Apollo Fox; Apollo Gyro AG1; Apollo Jet ...
The Apollo Guidance Computer software influenced the design of Skylab, Space Shuttle and early fly-by-wire fighter aircraft systems. [28] [29] The Apollo Guidance computer has been called "The fourth astronaut" for its role in helping the three astronauts who relied on it: Neil Armstrong, Buzz Aldrin and Michael Collins. [30]
The AJ10-137 engine (20,500 lbf (91 kN) of thrust) was used in the Apollo service module's service propulsion system from first flight in 1966. Trans-Earth injection, from lunar orbit, was the most critical usage of this engine during the Apollo program .
Apollo Command Module primary guidance system components Apollo Lunar Module primary guidance system components Apollo Inertial Measurement Unit. The Apollo primary guidance, navigation, and control system (PGNCS, pronounced pings) was a self-contained inertial guidance system that allowed Apollo spacecraft to carry out their missions when communications with Earth were interrupted, either as ...