Results 111 to 120 of about 69,089 (320)

Combustion Instability of Liquid Rocket Engines [PDF]

, 2004
D. K. Sung, Hwanil Huh, Chae-Hoon Sohn
openalex   +1 more source

Cryogenic gel flow viscometer [PDF]

, 1972
Coiled section of tubing measures viscous properties of gelled cryogenic propellants under conditions closely resembling flow in rocket engine systems. Characteristic flow curve provides data necessary for the design of prototype hardware systems using ...
Globus, R. H., Vanderwall, E. M.
core   +1 more source

Optimal Design of Fuel-Rich Gas Generator for Liquid Rocket Engine [PDF]

, 2004
Sun-Tak Kwon, Changjin Lee
openalex   +1 more source

Recurrent Neural Network based Soft Sensor for flow estimation in Liquid Rocket Engine Injector calibration

Flow Measurement and Instrumentation, 2021
Gilbert Chandra D., Vinoth B., S. U., Uma G., Umapathy M.   +4 more
semanticscholar   +1 more source

Demonstrated survivability of a high temperature optical fiber cable on a 1500 pound thrust rocket chamber [PDF]

A demonstration of the ability of an existing optical fiber cable to survive the harsh environment of a rocket engine was performed at the NASA Lewis Research Center.
Sovie, Amy L.
core   +1 more source

Design criteria monograph on turbopump systems [PDF]

, 1975
Turbopump assembly for modern liquid propellant rocket engine is complete system in itself. It consists of many components, some of which are themselves subsystems.

core   +1 more source

Overview and analysis of the experimentally measured throat heat transfer in liquid rocket engine thrust chambers

Acta Astronautica, 2021
M. Pizzarelli
semanticscholar   +1 more source

Ablative response of a silica phenolic to simulated liquid propellant rocket engine operating conditions [PDF]

Ablative response of silica phenolic to simulated liquid propellant rocket engine operating ...
Moyer, C. B., Powars, C. A., Rindal, R. A., Wool, M. R.   +3 more
core   +1 more source

Design criteria monograph for high-load high-speed rolling-contact bearings [PDF]

, 1972
Monograph was published which summarizes and systematically orders large body of successful techniques and practices developed for design of liquid rocket engine turbopump bearings.

core   +1 more source

Increasing the efficiency and stability of fuel supply to the combustion chamber of a liquid rocket engine by spray nozzles

Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение
In this paper, various configurations of jet nozzles are analyzed, as well as their design. The effects of the inlet chamfer of jet nozzles on their flow rate and range are considered.
Yu. I. Ageenko, A. S. Bubnova
doaj   +1 more source