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固体燃料超燃冲压发动机原理性试验研究

杨向明 刘伟凯 陈林泉 郑凯斌

固体火箭技术2012,Vol.35Issue(3):319-324,6.
固体火箭技术2012,Vol.35Issue(3):319-324,6.

固体燃料超燃冲压发动机原理性试验研究

Experiment study on the principle of solid fuel scramjet

杨向明 1刘伟凯 1陈林泉 1郑凯斌1

作者信息

  • 1. 中国航天科技集团公司四院四十一所,西安710025
  • 折叠

摘要

Abstract

Solid fuel scramjet was investigated by experiment. Ignition and combustion experiments that include solid hydrocarbon fuel and PMMA fuel were successfully done,which proved reliable ignition of the solid fuel in supersonic flow and stable combustion of the flame. Finally supersonic chamber characteristics of solid fuel were obtained. Combustion of PMMA fuel in supersonic flow was also investigated,and its regression rule was analyzed. Results show that regression rate of PMMA fuel changes with time, combustion outline tends to be plane and combustion region exhibits column.

关键词

超燃冲压发动机/固体燃料/超音速燃烧/原理性实验

Key words

scramjet/solid fuel/supersonic combustion/principle experiment

分类

航空航天

引用本文复制引用

杨向明,刘伟凯,陈林泉,郑凯斌..固体燃料超燃冲压发动机原理性试验研究[J].固体火箭技术,2012,35(3):319-324,6.

基金项目

航天科技集团科技创新研发项目. ()

固体火箭技术

OA北大核心CSCDCSTPCD

1006-2793

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