Principles of Space Instrument Design (Cambridge Aerospace Series, Series Number 9) (Volume 0)

Cruise, A. M.; Bowles, J. A.; Patrick, T. J.; Goodall, C. V.

ISBN 10: 052102594X / ISBN 13: 9780521025942

Published by Cambridge University Press, 2006

About this Item

Seller Inventory # I-9780521025942

Bibliographic Details

• Title: Principles of Space Instrument Design (Cambridge Aerospace Series, Series Number 9) (Volume 0)
• Publisher: Cambridge University Press
• Publication Date: 2006
• Language: English
• ISBN 10: 052102594X
• ISBN 13: 9780521025942
• Binding: Soft cover
• Condition: New

About this title

Synopsis

This informative account of the design of instruments used in rockets and spacecraft begins by introducing the basic principles of designing for the space environment. Following chapters discuss mechanical, structural, thermal and electronic design, including the problems that are frequently encountered in the testing and verification of spacecraft subsystems. The authors carefully describe important aspects of design, including stress analysis, multilayer insulation, two-dimensional sensor systems, mechanisms, the structure of space optics, and project management and control. A final chapter looks toward future developments of space instrument design and addresses issues arising from financial constraints. The book contains lists of symbols, acronyms and units and a comprehensive reference list. Worked examples, found throughout the text, make it valuable to final year undergraduate and beginning graduate students of physics, space science, space-craft engineering and astronautics.

Book Description

Designing an experiment to be performed in space involves highly complex techniques. There are considerable constraints, such as finding materials that are 'spaceworthy', limits on power, cost and manpower. This book provides a clear and comprehensive account of the techniques involved. Beginning with a chapter introducing the basic principles of designing for the space environment, following chapters discuss core elements of des ign including the problems that are frequently encountered in the testing and verification of spacecraft subsystems. Important topics are described including stress analysis, mechanisms and project management. A final chapter looks towards future developments of space instrument design. Worked examples are found throughout the text.