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Journal of Projectiles, Rockets, Missiles and Guidance >

2020 , Vol. 40 >Issue 3: 55 - 59

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2020.03.014

Research on Flight Application of Turbocharged Solid Propellant Ramjet

  • CHEN Sha 1 ,
  • YANG Yun 2 ,
  • LI Jiang 3 ,
  • LIU Kai 3
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  • 1 National Key Laboratory of Combustion Flow and Thermo-structure, Xi’an Insitute of Aerospace Propulsion Technology, Xi’an 710025, China
  • 2 The Fourth Academy of CSAC, Xi’an 710025, China
  • 3 National Key Laboratory of Combustion Flow and Thermo-structure, Northwestern Polytechnical University, Xi’an 710072, China

Received date: 2018-11-21

  Online published: 2025-02-12

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Abstract

In order to test whether the TSPR-powered tactical aircraft can achieve the intended mission objectives, taking HARM missile as research object, this paper carried on the design and the trajectory of the TSPR-driven HARM missile. It is concluded that the total mass of TSPR which is series connection is about 180 kg and the total length is 3.55 m. The TSPR-driven HARM missile can accelerate from (3 km、Ma 0.9) to cruise state (10 km、Ma 2.2), with a total range of 280.6 km, which is 3.9 times the range of the same quality solid rocket motor drive, and the average speed is about 1.1 times that of the solid rocket motor. It is proved that TSPR is an excellent tactical aircraft propulsion system.

Key words： turbocharged solid propellant ramjet; HARM missile; component design; flight trajectory

Cite this article

CHEN Sha , YANG Yun , LI Jiang , LIU Kai . Research on Flight Application of Turbocharged Solid Propellant Ramjet[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2020 , 40(3) : 55 -59 . DOI: 10.15892/j.cnki.djzdxb.2020.03.014

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