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Liquid Acquisition Devices for Advanced In-Space Cryogenic Propulsion Systems [Kietas viršelis]

(Propellants and Propulsion, NASA Glenn Research Center, Cleveland, OH, USA)
  • Formatas: Hardback, 488 pages, aukštis x plotis: 235x191 mm, weight: 1180 g
  • Išleidimo metai: 27-Nov-2015
  • Leidėjas: Academic Press Inc
  • ISBN-10: 0128039892
  • ISBN-13: 9780128039892
Kitos knygos pagal šią temą:
Liquid Acquisition Devices for Advanced In-Space Cryogenic Propulsion SystemsDidesnis paveikslėlis
  • Formatas: Hardback, 488 pages, aukštis x plotis: 235x191 mm, weight: 1180 g
  • Išleidimo metai: 27-Nov-2015
  • Leidėjas: Academic Press Inc
  • ISBN-10: 0128039892
  • ISBN-13: 9780128039892
Kitos knygos pagal šią temą:
Pastovi nuoroda: https://www.kriso.lt/db/9780128039892.html
Raktažodžiai:

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.

  • Presents a definitive reference for design ideas, analysis tools, and performance data on cryogenic liquid acquisition devices
  • Provides historical perspectives to present fundamental design models and performance data, which are applied to two practical examples throughout the book
  • Describes a series of models to optimize liquid acquisition device performance, which are confirmed through a variety of parametric component level tests
  • Includes video clips of experiments on a companion website

Daugiau informacijos

This book is a comprehensive work on the design and development of liquid acquisition devices for advanced cryogenic liquid propulsion systems that contains detailed component level and full scale cryogenic performance data, and a storehouse of design tools for modeling such complex cryogenic two-phase systems.
Foreword xiii
Preface xv
Acknowledgments xvii
1 Introduction
1(14)
1.1 The Flexible Path
1(2)
1.2 Fundamental Cryogenic Fluids
3(2)
1.3 Motivation for Cryogenic Propulsion Technology Development
5(1)
1.4 Existing Challenges with Cryogenic Propellants
5(1)
1.5 Cryogenic Fluid Management Subsystems
6(1)
1.6 Future Cryogenic Fluid Management Applications
7(4)
1.7 Purpose of Work and Overview by
Chapter
11(4)
2 Background and Historical Review
15(30)
2.1 Propellant Management Device Purpose
16(2)
2.2 Other Types of Propellant Management Devices
18(3)
2.3 Vanes
21(4)
2.4 Sponges
25(5)
2.5 Screen Channel Liquid Acquisition Devices
30(12)
2.6 Propellant Management Device Combinations
42(1)
2.7 NASA's Current Needs
42(3)
3 Influential Factors and Physics-Based Modeling of Liquid Acquisition Devices
45(42)
3.1 1-g One Dimensional Simplified Pressure Drop Model
46(2)
3.2 The Room Temperature Bubble Point Pressure
48(12)
3.3 Hydrostatic Pressure Drop
60(1)
3.4 Flow-Through-Screen Pressure Drop
61(6)
3.5 Frictional and Dynamic Pressure Drop
67(5)
3.6 Wicking Rate
72(3)
3.7 Screen Compliance
75(3)
3.8 Material Compatibility
78(1)
3.9 The Room Temperature Reseal Pressure Model
79(3)
3.10 Pressurant Gas Type
82(1)
3.11 Concluding Remarks and Implications for Cryogenic Propulsion Systems
83(4)
4 Room Temperature Liquid Acquisition Device Performance Experiments
87(24)
4.1 Pure Fluid Tests
88(8)
4.2 Binary Mixture Tests
96(9)
4.3 Reseal Pressure Tests
105(1)
4.4 Wicking Rate Tests
106(4)
4.5 Concluding Remarks
110(1)
5 Parametric Analysis of the Liquid Hydrogen and Nitrogen Bubble Point Pressure
111(32)
5.1 Test Purpose and Motivation
112(1)
5.2 Experimental Design
112(7)
5.3 Experimental Methodology
119(2)
5.4 Experimental Results and Discussion
121(21)
5.5 Concluding Remarks
142(1)
6 High-Pressure Liquid Oxygen Bubble Point Experiments
143(24)
6.1 Test Purpose and Motivation
143(2)
6.2 Experimental Design
145(4)
6.3 Experimental Methodology
149(1)
6.4 Experimental Results and Discussion
150(15)
6.5 Concluding Remarks
165(2)
7 High-Pressure Liquid Methane Bubble Point Experiments
167(36)
7.1 Test Purpose and Motivation
168(1)
7.2 Experimental Design
168(6)
7.3 Experimental Results and Discussion
174(4)
7.4 Thermal Analysis
178(22)
7.5 Concluding Remarks
200(3)
8 Warm Pressurant Gas Effects on the Static Bubble Point Pressure for Cryogenic Liquid Acquisition Devices
203(12)
8.1 Test Purpose and Motivation
203(2)
8.2 Design Modifications
205(1)
8.3 Experimental Methodology
206(1)
8.4 Test Matrix
207(1)
8.5 Warm Pressurant Gas Liquid Hydrogen Experiments
207(4)
8.6 Warm Pressurant Gas Liquid Nitrogen Experiments
211(3)
8.7 Concluding Remarks
214(1)
9 Full-Scale Liquid Acquisition Device Outflow Tests in Liquid Hydrogen
215(46)
9.1 Test Purpose and Motivation
216(1)
9.2 Test Plan
217(1)
9.3 Facility and Test Article
217(6)
9.4 Horizontal Liquid Acquisition Device Tests
223(3)
9.5 Flow-Through-Screen Tests
226(9)
9.6 1-g Inverted Vertical Liquid Acquisition Device Outflow Tests
235(24)
9.7 Concluding Remarks
259(2)
10 The Bubble Point Pressure Model for Cryogenic Propellants
261(28)
10.1 Current Model Limitations
261(2)
10.2 Summary of Data
263(1)
10.3 Room Temperature Pore Diameter Model
264(6)
10.4 Pressurant Gas Model
270(4)
10.5 Liquid Subcooling Model
274(5)
10.6 Warm Pressurant Gas Model
279(4)
10.7 Concluding Remarks
283(6)
11 The Reseal Point Pressure Model for Cryogenic Propellants
289(14)
11.1 Current Model Limitations
289(1)
11.2 Summary of Data
290(1)
11.3 Room Temperature Reseal Diameter Model
290(2)
11.4 Pressurant Gas Model
292(3)
11.5 Liquid Subcooling Model
295(3)
11.6 Warm Pressurant Gas Model
298(1)
11.7 Model Summary and Performance
299(1)
11.8 Concluding Remarks
300(3)
12 Analytical Model for Steady Flow through a Porous Liquid Acquisition Device Channel
303(26)
12.1 One-Dimensional Pressure Drop Model Drawbacks
304(1)
12.2 Evolution of the Solution Method
305(2)
12.3 Analytical Model Formulation
307(6)
12.4 Model Results, Sensitivities, and Comparison to One-Dimensional Model
313(9)
12.5 Dynamic Bubble Point Model
322(4)
12.6 Convective Cooling of the Liquid Acquisition Device Screen
326(1)
12.7 Concluding Remarks
327(2)
13 Optimal Liquid Acquisition Device Screen Weave for a Liquid Hydrogen Fuel Depot
329(14)
13.1 Background and Mission Requirements
330(2)
13.2 Bubble Point Pressure and Flow-through-Screen Pressure Drop
332(2)
13.3 Critical Mass Flux
334(1)
13.4 Minimum Bubble Point
335(1)
13.5 Minimum Screen Area
336(3)
13.6 Other Considerations
339(1)
13.7 Channel Number and Size
340(1)
13.8 Concluding Remarks
341(2)
14 Optimal Propellant Management Device for a Small-Scale Liquid Hydrogen Propellant Tank
343(28)
14.1 Background and Mission Requirements
344(1)
14.2 Analytical Screen Channel Flow Model in Microgravity
345(11)
14.3 Analytical Vane Model in Microgravity
356(4)
14.4 Trade Study Variables
360(2)
14.5 Trade Study Results
362(6)
14.6 Concluding Remarks
368(3)
15 Conclusions
371(6)
15.1 Summary
371(3)
15.2 Future Work
374(3)
Appendix A Historical Depot Demonstration Missions 377(6)
Appendix B Summary of Previously Reported Bubble Point Data 383(6)
Appendix C Langmuir Isotherm for the Liquid/Vapor Case 389(4)
Appendix D Langmuir Isotherms for the Solid/Liquid and Solid/Vapor Cases 393(4)
Appendix E Historical Heated Pressurant Gas Liquid Acquisition Device Tests 397(6)
Appendix F Previously Reported Porous Channel Solutions 403(8)
Appendix G Design Logic 411(4)
Glossary 415(6)
Bibliography 421(38)
Index 459
Dr. Jason Hartwig is a research aerospace engineer in the Propellants and Propulsion branch at the NASA Glenn Research Center in Cleveland, OH and is the lead technologist for cryogenic propellant transfer for the Agency. Jason has a BS in Physics, an MS in Mechanical Engineering, and a Doctorate in Aerospace Engineering from Case Western Reserve University. Hes been the PI on multiple cryogenic propulsion test programs at Glenn (CFM, PCAD, CPST, eCryo). Jason has 10 years of experience in the areas of cryogenic engineering, laser diagnostics, combustion, and propulsion. Jasons areas of expertise include design analysis and testing of cryogenic propellant management devices, line and tank chill and fill techniques, two phase cryogenic flow boiling and fluid mechanics, tank pressurization systems, and passive multi-layer insulation systems. Dr. Hartwig is also actively involved at NASA and Case in training and mentoring students through various programs.