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... .H. Przybilski '''Co-Author(s)''' - '''JBIS Volume ''' - Contents of the Journal of the British Interplanetary Society for Volume 55 55 '''Page ''' - 404-427 '''Year''' - 2002 '''Keywords''' - German rocket engines, German rocket experts, Soviet rocket genesis '''JBIS Reference Code ''' - 2002.55.404 '''Number of Pages''' - 24 Abstract A more accurate picture of the genesis of post-war Soviet rocket propulsion can ...

... projects, rocket engine, amateur altitude record, design, tests '''JBIS Reference Code ''' - 2009.62.211 '''Number of Pages''' - 8 Abstract This paper presents the results of the first DEIMOS Liquid Methane/Oxygen rocket engine test campaign. DEIMOS is an acronym for `Delft Experimental Methane Oxygen propulsion System'. It is a project performed by students under the auspices of DARE (Delft Aerospace Rocket Engineering). The engine provides ...

... gaseous propellant rocket engine. It is an undertaking of the authors, performed on project basis with fellow aerospace engineering students under auspices of DARE (Delft Aerospace Rocket Engineering). This paper describes the requirements, the engine development, and the design considerations and calculations as they were performed. Furthermore, the plans for engine tests ...

... rocket engines, Russian rocket engines, Valentin Glushko, OKB-456, NPO Energomash '''JBIS Reference Code ''' - 2001.54.311 '''Number of Pages''' - 24 Abstract Valentin P. Glushko (1908-89) oversaw the most influential rocket engine ... has developed more than 120 engines since the end of World War II 1 . This article will attempt to summarize the development of engines at the Glushko Design ...

... the British Interplanetary Society for Volume 64 64 '''Page ''' - 29-37 '''Year''' - 2011 '''Keywords''' - Nuclear Rocket Engine, Reactor Environments, Non-Nuclear Testing, Fissile Fuel Development '''JBIS Reference Code ''' - 2011.64.29 '''Number ... simulator was recently developed and commissioned for long duration hot hydrogen exposure of nuclear thermal rocket materials. This newly established non-nuclear testing capability uses a high-power, multi-gas, wall ...

... Image:OR-2-2.jpg 100px The "10" was a liquid fuel engine designed for the GIRD-X in 1933 by Fridrikh Zander . It had 70kg thrust and ... of 8 to 10 atm. Burn time was 22 seconds using 78% ethyl alcohol. Category:Rocket Engine

... Col. Glenn and Robert IL Gilruth. Third successful static-test firing of "Old Salty"—an H-1 rocket engine H-1 engine that had been submerged in salt water for four hours before each of its test ... of new engines. Early results indicated that engines could be recovered and rebuilt at a cost of about 10% of new engines. NASA fired a Scout rocket from Wallops Station , Va. The rocket flew 135 ...

... the 1.5-million lb. (680,389 kg) F-1 rocket engine that propelled the first stages of Saturn V missions to the Moon. A closer examination of the respective histories of the F-1 rocket engine ... -Ziegert, Stadt Dortmund, Institut für Zeitungsforschung (Institute for Newspaper Research), 3 May 1980, to Frank H. Winter, copy in “Germany, 1930-1934” file, NASM. note 7 Letter, W.L ...

... House for the President's signature. House passed Independent Offices Appropriation Bill for 1963 (H.R. 12711) containing an amendment providing for 25% indirect costs on research grants ... plans to expand its Canoga Park, Calif., facilities to manufacture F-1 rocket engine F-1 and J-2 rocket engine J-2 rocket engines for NASA’s Advanced Saturn launch vehicle. Four American scientists led ...

... Launch System (SLS). The awardees will develop engineering demonstrations and risk reduction concepts for a future version of the SLS, a heavy-lift rocket that will provide an entirely new capability for ... test several primary components of the F-1 rocket engine originally developed for the Apollo Program, including an integrated powerpack, the primary rotating machinery of the engine. Additionally, the contract will demonstrate innovative fabrication ...

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