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... 64 '''Page ''' - 29-37 '''Year''' - 2011 '''Keywords''' - Nuclear Rocket Engine, Reactor Environments, Non-Nuclear Testing, Fissile Fuel Development '''JBIS Reference ... hydrogen exposure of nuclear thermal rocket materials. This newly established non-nuclear testing capability uses a high-power, multi-gas, wall-stabilised constricted arc-heater to produce high-temperature pressurised hydrogen ...

... 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 ...

... ''' - Soviet 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 design organization in the Soviet Union. Originally known as OKB-456, the design bureau designed first stage engines for almost all operational Soviet ICBMs, the ...

... '''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 ...

... 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

... The Nuclear Rocket with the idea of creating a solar system transportation plan with different nuclear rockets operating like ... useful when comparing a chemical rocket engine with another or with an airplane engine with another, but here it ... hydrogen molecule into two atoms, or call it the use of monatomic hydrogen. Throwing a single hydrogen atom out the nozzle is stunning because now in our rocket ...

... rockets b. solid-fueled chemical rockets c. hybrid-fuel rockets d. steam rockets e. cold gas rockets f. electric thermal rockets g. solar thermal rockets h. nuclear thermal rockets i. electric ion thrusters, and many more. a. Liquid chemical rocket engines ...

... s book "Hector Servadac's Adventures on his Journey Through the Solar World" which fascinated him even more than the "Trip to ... and are subjected to the necessary tests. As described in Oberth, hydrogen and oxygen are the fuels used. Here, the researchers relied ... designation "A1" Ley jumped years into the future. For the first rocket engine, which was tested by Wernher von Braun in early 1933, was ...

... Rocket Propellants 10 - Liquid Propellant Rocket Power Plants 26 - Liquid Rocket Motor Testing 45 - 73 March 1948 - Rocket Motors Project Heavy Steel Cables 5 - Present and Future of Rockets 9 - The Acid-Aniline Rocket Engine ...

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