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Heat transfer / Chemical engineering / Rocket propulsion / Heat conduction / Liquid-propellant rocket / Rocket engine / Heat exchanger / Gas / Heat capacity / Chemistry / Physics / Thermodynamics


GLUC[removed]A PRESSURIZED SYSTEMS OF THE TANKS. Author: Prof. Alexander A. Kozlov Moscow Aviation Institute (State Technical University), Moscow, Russia
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Document Date: 2010-06-18 12:21:53


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File Size: 907,16 KB

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Facility

Ms. Lera Chadova Moscow Aviation Institute / Prof. Alexander A. Kozlov Moscow Aviation Institute / State Technical University / /

IndustryTerm

liquid rocket engine device / carrier rocket / gas generators pressurization working / carrier tank / energy conservation / displacement high-boiling hot gas component / flange inlet gas generator gas / gas volume / inlet gas generator gas / gas cap starts flowing gas / exit device / tank carrier rocket / space transport systems / gas-vapor volume / rocket engine devices / generated gas / hot oxidative gas / pneumatic systems / interface gas / gas ball / entrance device / gas generators / reach fuel generator gas / pressurized gas / energy / occurring in the gas-vapor volume / /

Organization

Ms. Lera Chadova Moscow Aviation Institute / Alexander A. Kozlov Moscow Aviation Institute / Moscow Aviation Institute / Technical University / /

Person

S.N.Konyukhova / Alexander A. Kozlov Moscow / Buena Vista Florida / A.A. Kozlov / V / /

Position

Editor / interface wb / Keeping wb / collector / Model / initial value RT / RT / Pressurized systems Keeping wb / tank pressurization Keeping wb / wb / producer / /

Product

Latte W10 Portable Audio Device / Apollo / A-50 / Titan / /

ProvinceOrState

New Mexico / /

Technology

AV / condensation / heat transfer / /

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