Results 101 to 110 of about 31,818 (301)
Summary of literature survey of hypergolic ignition spike phenomena, phase I Final report, Apr. 8 - Dec. 31, 1965 [PDF]
Summary of industry survey and literature search of ignition spike phenomena in low thrust, hypergolic, liquid bipropellant rocket ...
Christos, T., Perlee, H. E.
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Aggregate, Volume 7, Issue 1, January 2026.Atomically precise metal nanoclusters are ultrasmall aggregates of metal atoms with finely tunable structures. They exhibit broad PL across visible to NIR wavelengths by tuning size, structure, and composition. The review addresses fundamental emission mechanisms and structure–property correlations, evaluating enhancement strategies (ligand ...
Xiuling Guo +4 more
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Liquid Hydrogen/Liquid Oxygen Rocket Engine Technology
Journal of the Korean Society of Propulsion Engineers, 2022 Nam-Kyung Cho +3 more
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Development Advances in Liquid Rocket Engines Turbopump: A Review
, 2023 Rahul Singhal +5 more
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Research on the comparative analysis of thrust and specific impulse performance - different cycle types of liquid rocket engines [PDF]
, 2023 Mingyu Mao
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Lithium Nitrate Effects for Lithium‐Based Chemical Batteries: A Review
Carbon Energy, Volume 8, Issue 1, January 2026.Lithium nitrate (LiNO3) has been widely used to address uneven Li plating/stripping and stabilize the Li/electrolyte interface, and to date, many strategies on how to use nitrates have been explored. This review focuses attention on the effects of LiNO3 in lithium‐based batteries, aiming to provide scientific guidance for the optimization of electrode ...
Xianshu Wang +8 more
wiley +1 more source
Thermal degradation of impact‐modified PMMA in mechanical and chemical recycling
The Canadian Journal of Chemical Engineering, Volume 104, Issue 1, Page 31-43, January 2026.Abstract Poly (methyl methacrylate) (PMMA) is a thermoplastic with outstanding tensile strength, UV resistance, and a high level of transparency that has been used widely for optical applications such as glazing in the automobile industry. Mechanical recycling, the most widespread method, degrades the physical properties and prevents reusing PMMA in ...
Tien Dat Nguyen +6 more
wiley +1 more source
Mehran University Research Journal of Engineering and Technology, 2019 Optimum characteristic length of the combustion chamber of liquid rocket engine is very important to get higher energy from the liquid propellants. Characteristic length is defined by the time required for complete burning of fuel.
Tajwali Khan, Ihtzaz Qamar
doaj
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.
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The physiology of survival: Space
Experimental Physiology, EarlyView.
Damian M. Bailey, Angelique van Ombergen
wiley +1 more source