Book Details
Format
Paperback / Softback
ISBN-10
3642094775
ISBN-13
9783642094774
Edition
Softcover reprint of hardcover 1st ed. 2008
Publisher
Springer-Verlag Berlin and Heidelberg GmbH & Co. KG
Imprint
Springer-Verlag Berlin and Heidelberg GmbH & Co. K
Country of Manufacture
DE
Country of Publication
GB
Publication Date
Oct 19th, 2010
Print length
504 Pages
Weight
802 grams
Dimensions
23.30 x 15.70 x 3.00 cms
Ksh 52,100.00
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General.- Design Process.- Launch Vehicle Systems.- Spacecraft Subsystems.- Design and Safety factors.- Spacecraft Design Loads.- Test Verification.- Design of Spacecraft structure.- Strength and Stiffness of Structural Elements.- Sandwich Construction.- Finite Element Analysis.- Stiffness/Flexibility Analysis.- Material Selection.- Spacecraft Mass.- Natural Frequencies, an Approximation.- Modal Effective Mass.- Dynamic Model Reduction Methods.- Dynamic Substructuring, Component Mode Synthesis.- Output Transformation Matrices.- Coupled Dynamic Loads Analysis.- Random Vibrations Simplified Response Analysis.- Fatigue Life Prediction.- Shock-Response Spectrum.- Damage to Spacecraft by Meteoroids and Orbital Debris.- Prescribed Averaged Temperatures.- Thermal-elastic Stresses.- Coefficients of thermal & moisture expansion.- Venting Holes.- Examples.
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