Name: Ionic Liquid Monopropellants for Advanced Propulsion
SKU: 195248456
Price: 61230 KRW
Availability: InStock
Author: Drishyam
ISBN: 9798256289751

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Ionic Liquid Monopropellants for Advanced Propulsion

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직수입양서 Ionic Liquid Monopropellants for Advanced Propulsion

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Drishyam

Indy Pub 2026.08.12.

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The development of advanced propulsion systems has increased interest in energetic materials that can provide reliable performance while offering improved handling, storage, and system-integration characteristics. Ionic Liquid Monopropellants for Advanced Propulsion provides a focused introduction to the chemistry, physical properties, energetic behavior, and engineering considerations associated with ionic-liquid-based monopropellants. The book brings together concepts from propulsion engineering, physical chemistry, thermodynamics, energetic materials, and materials science within a structured technical framework.The book introduces the fundamental characteristics of ionic liquids and explains why their distinctive physicochemical properties make them relevant to advanced propulsion research. Readers are introduced to concepts including ionic structure, vapor pressure, density, viscosity, thermal stability, decomposition behavior, energy content, and chemical compatibility. These properties provide the foundation for understanding how ionic liquids can be considered for propulsion applications and how molecular structure can influence their physical and energetic characteristics.A central focus is placed on ionic liquid monopropellants and their relationship to propulsion-system requirements. The text examines the general principles of monopropellant decomposition, energy release, thermochemical performance, combustion products, thermal behavior, and propulsion-system integration. Attention is given to the relationship between propellant composition, physical properties, energetic characteristics, and theoretical propulsion performance.The book further explores important considerations in evaluating ionic liquid monopropellants, including thermochemical analysis, density-specific impulse relationships, decomposition temperature, stability, storage characteristics, and material compatibility. These factors are discussed as part of the broader engineering challenge of developing propellant systems that balance energetic performance with practical handling and operational requirements.

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