An Overview on Development of Small Turbine Engines for Missiles
To provide superior cruise thrust for high subsonic intermediate-long range missiles, small turbojet and turbofan engines have become the competitive focus for military powers. The turbine engines for missiles are characteristic of low cost, short life, small size, high speed, low pressure ratio, se...
| Main Authors: | , , |
|---|---|
| Format: | Article |
| Language: | zho |
| Published: |
Editorial Department of Advances in Aeronautical Science and Engineering
2018-02-01
|
| Series: | Hangkong gongcheng jinzhan |
| Subjects: | |
| Online Access: | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2017074?st=article_issue |
| _version_ | 1797990767103311872 |
|---|---|
| author | Xue Ranran Li Fengchao Ren Lilei |
| author_facet | Xue Ranran Li Fengchao Ren Lilei |
| author_sort | Xue Ranran |
| collection | DOAJ |
| description | To provide superior cruise thrust for high subsonic intermediate-long range missiles, small turbojet and turbofan engines have become the competitive focus for military powers. The turbine engines for missiles are characteristic of low cost, short life, small size, high speed, low pressure ratio, severe volumetric heat release rate and various starting or ignition methods. They are widely equipped on strategic and tactical weapons, such as cruise, anti-ship and air-to-ground missiles. The development situation of small turbine engines within 100～700 daN since 1970 s is summarized and analyzed comprehensively, including well-known products, main technical parameters, basic features, application status and development trend. The study can provide references for the research work on missile propulsion systems. Lower cost, less fuel consumption and fewer parts will be the future goals. The Propfan engines have advantages of nice high subsonic performance and low fuel consumption, and the pulse detonation turbine engines possess high thermodynamic cycle efficiency and simple structure. They are both important development directions of advanced turbine engines for missiles. |
| first_indexed | 2024-04-11T08:40:36Z |
| format | Article |
| id | doaj.art-11bd864e8afa4166ae3f593c35acec4b |
| institution | Directory Open Access Journal |
| issn | 1674-8190 |
| language | zho |
| last_indexed | 2024-04-11T08:40:36Z |
| publishDate | 2018-02-01 |
| publisher | Editorial Department of Advances in Aeronautical Science and Engineering |
| record_format | Article |
| series | Hangkong gongcheng jinzhan |
| spelling | doaj.art-11bd864e8afa4166ae3f593c35acec4b2022-12-22T04:34:12ZzhoEditorial Department of Advances in Aeronautical Science and EngineeringHangkong gongcheng jinzhan1674-81902018-02-0191182710.16615/j.cnki.1674-8190.2018.01.00320180103An Overview on Development of Small Turbine Engines for MissilesXue Ranran0Li Fengchao1Ren Lilei2Aero Engine Academy of China, Aero Engine Corporation of China, Beijing 101304, ChinaAero Engine Academy of China, Aero Engine Corporation of China, Beijing 101304, ChinaAero Engine Academy of China, Aero Engine Corporation of China, Beijing 101304, ChinaTo provide superior cruise thrust for high subsonic intermediate-long range missiles, small turbojet and turbofan engines have become the competitive focus for military powers. The turbine engines for missiles are characteristic of low cost, short life, small size, high speed, low pressure ratio, severe volumetric heat release rate and various starting or ignition methods. They are widely equipped on strategic and tactical weapons, such as cruise, anti-ship and air-to-ground missiles. The development situation of small turbine engines within 100～700 daN since 1970 s is summarized and analyzed comprehensively, including well-known products, main technical parameters, basic features, application status and development trend. The study can provide references for the research work on missile propulsion systems. Lower cost, less fuel consumption and fewer parts will be the future goals. The Propfan engines have advantages of nice high subsonic performance and low fuel consumption, and the pulse detonation turbine engines possess high thermodynamic cycle efficiency and simple structure. They are both important development directions of advanced turbine engines for missiles.http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2017074?st=article_issueaero-engineturbine enginesmall sizedmissilepropfanpulse detonation |
| spellingShingle | Xue Ranran Li Fengchao Ren Lilei An Overview on Development of Small Turbine Engines for Missiles Hangkong gongcheng jinzhan aero-engine turbine engine small sized missile propfan pulse detonation |
| title | An Overview on Development of Small Turbine Engines for Missiles |
| title_full | An Overview on Development of Small Turbine Engines for Missiles |
| title_fullStr | An Overview on Development of Small Turbine Engines for Missiles |
| title_full_unstemmed | An Overview on Development of Small Turbine Engines for Missiles |
| title_short | An Overview on Development of Small Turbine Engines for Missiles |
| title_sort | overview on development of small turbine engines for missiles |
| topic | aero-engine turbine engine small sized missile propfan pulse detonation |
| url | http://hkgcjz.cnjournals.com/hkgcjz/article/abstract/2017074?st=article_issue |
| work_keys_str_mv | AT xueranran anoverviewondevelopmentofsmallturbineenginesformissiles AT lifengchao anoverviewondevelopmentofsmallturbineenginesformissiles AT renlilei anoverviewondevelopmentofsmallturbineenginesformissiles AT xueranran overviewondevelopmentofsmallturbineenginesformissiles AT lifengchao overviewondevelopmentofsmallturbineenginesformissiles AT renlilei overviewondevelopmentofsmallturbineenginesformissiles |