Summary
In order to acquire the knowledge on the dynamic characteristics of the solid propellant launch vehicle and to assess the dynamic environment of the satellite or installed electronics, two kinds of study have been carried out. The one is measurement of the response of the actual vehicle in flight and the other is an analytical and experimental approach to the shock and vibration characteristics of small test rocket segments containing solid propellant.
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© 1979 Springer-Verlag, Berlin/Heidelberg
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Mori, D., Onoda, J. (1979). Shock and Vibration Characteristic of Solid Rocket Vehicles. In: Kawata, K., Shioiri, J. (eds) High Velocity Deformation of Solids. International Union of Theoretical and Applied Mechanics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-67208-8_34
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DOI: https://doi.org/10.1007/978-3-642-67208-8_34
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-67210-1
Online ISBN: 978-3-642-67208-8
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