Results 71 to 80 of about 69,089 (320)
Injector element characterization methodology [PDF]
Characterization of liquid rocket engine injector elements is an important part of the development process for rocket engine combustion devices. Modern nonintrusive instrumentation for flow velocity and spray droplet size measurement, and automated ...
Cox, George B., Jr.
core +1 more source
Laminar flow enhancement Patent [PDF]
Laminar flow of liquid coolants in rocket ...
Ayvazian, R. A.
core +1 more source
Recent Advances in Non‐Aqueous Liquid Electrolytes for High‐Voltage Sodium‐Ion Batteries
Increasing charging voltage is an effective way to realize sodium‐ion batteries with low cost and high energy density. This review systematically summarizes the development of electrolytes for high‐voltage sodium‐ion batteries in recent years, aiming to promote the breakthrough and application of high energy density sodium‐ion batteries.
Jing Ning+9 more
wiley +1 more source
Statistical derivation of design criteria for liquid rocket combustion instability Final report [PDF]
Statistical correlation between engine design and combustion stability in liquid propellant rocket ...
Bastress, E. K.+2 more
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Annular rocket motor and nozzle configuration Patent [PDF]
High thrust annular liquid propellant rocket engine and exhaust nozzle ...
Connors, J. F.
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This review presents recent advances in intelligent inspection robots for structural health monitoring. It highlights key technologies in sensing, data processing, and fault localization, along with challenges and future directions. The aim is to support practical deployment and promote intelligent, efficient, and autonomous monitoring systems ...
Dongjie Li+6 more
wiley +1 more source
Combustion instability research Summary report, 1970 [PDF]
Combustion instability in liquid rocket ...
Bracco, F. V.+9 more
core +1 more source
Nondestructive testing of brazed rocket engine components [PDF]
Report details study made of nondestructive radiographic, ultrasonic, thermographic, and leak test methods used to inspect and evaluate the quality of the various brazed joints in liquid-propellant rocket engine components and assemblies. Descriptions of
Adams, C. J.+2 more
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Abstract We investigated in situ ionospheric plasma density perturbations triggered by the South Korea KSLV‐2 rocket launches on 21 June 2022, and 25 May 2023, by combining ground‐based GNSS total electron content (TEC) observations with in situ measurements from the FORMOSAT‐7/COSMIC‐2 Ion Velocity Meter (IVM).
Jong‐Min Choi+7 more
wiley +1 more source
This paper presents the activities in the area of liquid propulsion, which received an effective boost at the end of the 90s.
Marco F. Carvalho Torres+4 more
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