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加速度对丁羟推进剂燃速影响的研究

郭彤 侯晓

火炸药学报2001,Vol.24Issue(1):30-32,3.
火炸药学报2001,Vol.24Issue(1):30-32,3.

加速度对丁羟推进剂燃速影响的研究

Study of the Acceleration Effects on the Burning Rate of HTPB Propellant

郭彤 1侯晓1

作者信息

  • 1. 中国航天科技集团公司第41研究所,
  • 折叠

摘要

Abstract

In the paper, the acceleration effects on the burning rate of HTPB propellant are presented. Through the experiments of motors in the acceleration field, the experimental data can be got, inclouding the effects of the acceleration level and the acceleration orientation. Then based on the phenomenological model and multi-flame of BOP model, the model of the burning rate augmentation in the acceleration field has been built. The experimental data and the model data are uniform. The model can be available for reference to the qualitative analysis of the design of SRM.

关键词

固体发动机/加速度/燃速/稳态燃烧模型

分类

航空航天

引用本文复制引用

郭彤,侯晓..加速度对丁羟推进剂燃速影响的研究[J].火炸药学报,2001,24(1):30-32,3.

火炸药学报

OA北大核心CSCD

1007-7812

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