A Study of the Viscoelasticity of a Solid Propellant
碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 94 === From theoretical point of view, time-temperature shift factors (log aT ) and failure time at constant TRUess (τ) of composite propellants can be estimated if their Ea, n and B are given. In addition, one of HTPB/AP/RDX/Al composite propellants was characteri...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2006
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| Online Access: | http://ndltd.ncl.edu.tw/handle/04441720751834351512 |