Citation: | HE Ye, LI Junwei, TIAN Zhongliang, et al. Effects of acceleration overload on combustion characteristics of HTPB/AP/Al propellant[J]. Journal of Aerospace Power, 2024, 39(8):20220067 doi: 10.13224/j.cnki.jasp.20220067 |
In order to study the effect of acceleration field on the combustion characteristics of HTPB/AP/Al propellant, an overload test rocket with both burning rate measurement and condensate product collection functions was designed. The effects of different overload magnitudes (−50
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