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... 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 ...

... '''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 ... and personal interviews with the German rocket experts who were taken to the USSR. For the first time it became clear that the raketnyje dvigateli (rocket engines) of even today's Soyuz launcher ...

... 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

... 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 ... companies launch our astronauts and their supplies from U.S. soil." ''MEDIA ADVISORY: M/12-196 NASA CHIEF TECHNOLOGIST VISITS EMERGENT SPACE TECH IN MARYLAND OCT. 15'' WASHINGTON ...

... of F-1 rocket engine was now "under control," in Missiles and Rockets. Installation of mechanical isolator separated oscillations in engine pump from oscillations in fuel system. "Since that time the engine has ... -Zeus antimissile missile performed successfully in development test at White Sands Missile Range , N.M. ''(M&R, 7/8/63,10)'' Dr. Robert W. Buchheim became USAF Chief Scientist, ...

... 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, as well as the third and second stage J-2 engines of the Saturn V, also shows they all descended from the same Redstone engine. ref 12 The first artificial satellite, '' Sputnik 1 ...

... 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 ...

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