aerodynamics of rocket

  • 81Douglas A-26 Invader — Not to be confused with B 26 Marauder. A 26 (B 26) Invader USAAF A 26B 35 DL (AAF Ser. No. 41 39456) Role …

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  • 82Messerschmitt Bf 109 variants — Main article: Messerschmitt Bf 109 Bf 109 Bf 109G 10, with Erla Haube canopy and taller, wooden vertical fin/rudd …

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  • 83Список награждённых Национальной медалью науки США — Джошуа Ледерберг (справа) получает Национальную медаль науки из рук Президента США Джорджа Буша старшего Список …

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  • 84aviation — I (New American Roget s College Thesaurus) Science of flight Nouns 1. (science of flight) aviation, flight, flying; navigation, aerial navigation; aeronautics, aerodynamics, aerodonetics, aerostatics, avionics, rocketry; aerial navigation,… …

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  • 85Sound barrier — In aerodynamics, the sound barrier usually refers to the point at which an aircraft moves from transonic to supersonic speed. The term came into use during World War II when a number of aircraft started to encounter the effects of compressibility …

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  • 86Rutan Long-EZ — The Rutan Model 61 Long EZ is a homebuilt aircraft with a canard layout designed by Burt Rutan s Rutan Aircraft Factory. It is derived from the VariEze, which was first offered to homebuilders in 1976. The prototype (… …

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  • 87James H. Kindelberger — James H. Dutch Kindelberger (May 8, 1895 July 27, 1962) was an American pioneer of aviation. He was also a leader of North American Aviation for a number of years. The International Aerospace Hall of Fame inducted Kindelberger in 1977. North… …

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  • 88Dryden Flight Research Center — Dryden Flight Research Center …

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  • 89Apollo Command/Service Module — Apollo CSM The Apollo 15 CSM in lunar orbit Description Role: Earth and Lunar Orbit Crew: 3; CDR, CM pilot, LM pilot Dimensions Height: 36.2 ft 11.03 m …

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  • 90Propelling nozzle — A propelling nozzle is a component of a jet engine that is found at the tail of the engine that operates to form an exhaust jet and to maximise the use of the exhaust gas s energy throughout the engine so that the maximum overall thrust is… …

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