rdf-syntax-grammar
mods:
  schema location: http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-2.xsd
  title info:
    title: Liquid acquisition devices for advanced in-space cryogenic propulsion systems
  name:
    name part: Hartwig, Jason William
    role:
      role term: creator
    role:
      role term: author.
  name:
    name part: ScienceDirect (Online service)
  type of resource: text
  genre: bibliography
  genre: Electronic books.
  origin info:
    place:
      place term: nyu
    date issued: 2016
    issuance: monographic
  language:
    language term: eng
  physical description:
    form: remote
    extent: 1 online resource
  abstract: Liquid Acquisition Devices for Advanced In-Space Cryogenic Propulsion Systems discusses the importance of reliable cryogenic systems, a pivotal part of everything from engine propulsion to fuel deposits. As some of the most efficient systems involve advanced cryogenic fluid management systems that present challenging issues, the book tackles issues such as the difficulty in obtaining data, the lack of quality data and models, and the complexity in trying to model these systems. The book presents models and experimental data based on rare and hard-to-obtain cryogenic data. Through clear descriptions of practical data and models, readers will explore the development of robust and flexible liquid acquisition devices (LAD) through component-level and full-scale ground experiments, as well as analytical tools. This book presents new and rare experimental data, as well as analytical models, in a fundamental area to the aerospace and space-flight communities. With this data, the reader can consider new and improved ways to design, analyze, and build expensive flight systems.
  table of contents: Front Cover; Liquid Acquisition Devices for Advanced In-Space Cryogenic Propulsion Systems; Copyright; Dedication; Contents; Foreword; Preface; Acknowledgments; Chapter 1: Introduction; 1.1. The Flexible Path; 1.2. Fundamental Cryogenic Fluids; 1.3. Motivation for Cryogenic Propulsion Technology Development; 1.4. Existing Challenges with Cryogenic Propellants; 1.5. Cryogenic Fluid Management Subsystems; 1.6. Future Cryogenic Fluid Management Applications; 1.6.1. In-Space Cryogenic Engines; 1.6.2. In-Space Cryogenic Fuel Depots; 1.7. Purpose of Work and Overview by Chapter
  table of contents: Chapter 2: Background and Historical Review2.1. Propellant Management Device Purpose; 2.2. Other Types of Propellant Management Devices; 2.3. Vanes; 2.3.1. Design Concept, Basic Flow Physics, and Principle of Operation; 2.3.2. Advantages and Disadvantages; 2.3.3. Storable Propellant Historical Examples; 2.3.3.1. Space Experiments; 2.3.3.2. Vehicles and Missions; 2.4. Sponges; 2.4.1. Design Concept, Basic Flow Physics, and Principle of Operation; 2.4.2. Advantages and Disadvantages; 2.4.3. Storable Propellant Historical Examples; 2.4.3.1. Space Experiments; 2.4.3.2. Vehicles and Missions
  table of contents: 2.5. Screen Channel Liquid Acquisition Devices2.5.1. Design Concept, Basic Flow Physics, and Principle of Operation; 2.5.2. Mesh and Metal Type; 2.5.3. Advantages and Disadvantages; 2.5.4. Storable Propellant Historical Examples; 2.5.4.1. Space Experiments; 2.5.4.2. Vehicles and Missions; 2.5.5. Cryogenic Propellant Historical Examples; 2.6. Propellant Management Device Combinations; 2.7. NASA's Current Needs; Chapter 3: Influential Factors and Physics-Based Modeling of Liquid Acquisition Devices; 3.1. 1-g One Dimensional Simplified Pressure Drop Model
  table of contents: 3.2. The Room Temperature Bubble Point Pressure3.2.1. Assumptions; 3.2.2. Bubble Point Model Derivation; 3.2.3. Types of Bubble Point Experiments; 3.2.4. Surface Tension Model; 3.2.5. Specifying the Effective Pore Diameter; 3.2.6. Previously Reported Bubble Points; 3.3. Hydrostatic Pressure Drop; 3.4. Flow-Through-Screen Pressure Drop; 3.4.1. Model Derivation; 3.4.2. Model Parameters and Flow-Through-Screen Experiment; 3.4.3. Historical Data and Trends; 3.5. Frictional and Dynamic Pressure Drop; 3.6. Wicking Rate; 3.6.1. Model Derivation; 3.6.2. Wicking Rate Experiment
  table of contents: 3.6.3. Historical Data and Trends3.7. Screen Compliance; 3.7.1. Model Derivation and Screen Compliance Experiment; 3.7.2. Historical Data and Trends; 3.8. Material Compatibility; 3.9. The Room Temperature Reseal Pressure Model; 3.9.1. Model Derivation; 3.9.2. Historical Data and Trends; 3.9.3. Specifying the Reseal Diameter; 3.10. Pressurant Gas Type; 3.11. Concluding Remarks and Implications for Cryogenic Propulsion Systems; Chapter 4: Room Temperature Liquid Acquisition Device Performance Experiments; 4.1. Pure Fluid Tests; 4.1.1. Scanning Electron Microscopy Analysis
  note: Jason William Hartwig.
  note: Includes bibliographical references and index.
  subject:
    topic: Liquid propellants
  subject:
    topic: Space vehicles
    topic: Propulsion systems
  subject:
    topic: Space vehicles
    topic: Design
  subject:
    topic: Propergols liquides
  subject:
    topic: Véhicules spatiaux
    topic: Propulsion
  subject:
    topic: TECHNOLOGY & ENGINEERING
    topic: Mechanical
  subject:
    topic: Liquid propellants
  subject:
    topic: Space vehicles
    topic: Design
  subject:
    topic: Space vehicles
    topic: Propulsion systems
  classification: TL783.4
  classification: 621.4356
  related item:
    title info:
      title: Liquid acquisition devices for advanced in-space cryogenic propulsion systems
    name:
      name part: Hartwig, Jason William.
    origin info:
      publisher: London, England : Academic Press, ©2016
    physical description:
      extent: xviii, 469 pages
  identifier: 9780128039908
  identifier: 0128039906
  identifier: 0128039892
  identifier: 9780128039892
  identifier: http://proxy.library.tamu.edu/login
  record info:
    record content source: N$T
    record creation date: 151223
    record change date: 20260407210820.5
    record identifier: in00005760096
    language of cataloging:
      language term: eng