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Spacecraft Thermal Control Handbook, Volume 2: Cryogenics (Aerospace Press)

جلد کتاب Spacecraft Thermal Control Handbook, Volume 2: Cryogenics  (Aerospace Press)

معرفی کتاب «Spacecraft Thermal Control Handbook, Volume 2: Cryogenics (Aerospace Press)» نوشتهٔ Martin Donabedian; American Institute of Aeronautics and Astronautics، منتشرشده توسط نشر AIAA (American Institute of Aeronautics & Astronautics) در سال 2002. این کتاب در فرمت pdf، زبان انگلیسی ارائه شده است.

The number of satellite systems that require some form of cryogenic cooling has grown enormously over the last several years. With so many engineers, scientists, and technicians working on cryogenic systems for the first time in their careers, the need for a single resource that touched on all the technologies relevant to cryogenics was apparent. The book includes 23 chapters--written by industry experts--that will help the reader in the design, analysis, integration, testing, and operation of a variety of instruments, sensors, and other devices that must be cooled to cryogenic temperatures. temperatures. Sections include: Stored Expandable Cooling Systems: Cryogenic Radiators and Radiant Coolers; Cryocoolers (Mechanical Refrigerators): Cryogenic Components, Transport, Storage, and Integration; Thermal Margins, Estimating Risks, and Lessons Learned; IR Sensor Thermal Modeling and Analysis; and Cooler Specifications and Material Properties.

The number of satellite systems that require some form of cryogenic cooling has grown enormously over the last several years. With so many engineers, scientists, and technicians working on cryogenic systems for the first time in their careers, the need for a single resource that touched on all the technologies relevant to cryogenics was apparent.

The book includes 23 chapters—written by industry experts—that will help the reader in the design, analysis, integration, testing, and operation of a variety of instruments, sensors, and other devices that must be cooled to cryogenic temperatures. Sections include: Stored Expendable Cooling Systems; Cryogenic Radiators and Radiant Coolers; Cryocoolers (Mechanical Refrigerators); Cryogenic Components, Transport, Storage, and Integration; Thermal Margins, Estimating Risks, and Lessons Learned; IR Sensor Thermal Modeling and Analysis; and Cooler Specifications and Material Properties.

Annotation This is a revised and updated of (1994) and has been expanded to discuss interplanetary spacecraft as well as Earth- orbiting satellites. The work is presented as a compendium of corporate knowledge in the field of thermal control of uncrewed spacecraft and was written for thermal engineers of a range of experience levels. After discussing general issues and historical design approaches chapters examine current thermal control hardware, the thermal design and testing process, and emerging thermal technologies. Annotation c. Book News, Inc., Portland, OR (booknews.com) Although spacecraft with components that must be cooled to cryogenic temperatures of 2 to 150 K have been flown since the 1960s, recent years have seen a substantial growth in the emerging number of programs that include such spacecraft to service scientific, military, and weather observation missions.
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