Regression rate and combustion performance investigation of...

Aerospace Science and Technology 2015 / 04 Vol. 42

Regression rate and combustion performance investigation of aluminum metallized HTPB/98HP hybrid rocket motor with numerical simulation

Sun, Xingliang, Tian, Hui, Yu, Nanjia, Cai, Guobiao
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Volume:
42
Language:
english
Journal:
Aerospace Science and Technology
DOI:
10.1016/j.ast.2015.01.014
Date:
April, 2015
File:
PDF, 2.35 MB
english, 2015
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