Turbocharged Solid Propellant Ramjet for Tactical Missile

Sa Yang; Guo Qiang He; Yang Liu; Jiang Li

doi:10.4028/www.scientific.net/AMM.152-154.204

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 152-154Turbocharged Solid Propellant Ramjet for Tactical...

Turbocharged Solid Propellant Ramjet for Tactical Missile

Abstract:

Turbocharged solid propellant ramjet (TSPR) is the combination of solid propellant gas generator air turbo ramjet (ATR)with solid ramjet, is cycle of augmented ATR, the parametric performance calculation were carried out for TSPR, The effects of independent design parameters including parameters of compressor and turbine and propellants were studied and the preferred compressor, turbine and propellants were obtained for TSPR; The operation envelop of TSPR and ATR were obtain under the preferred component limitation, the results shows that TSPR offers wide speed-altitude operation envelope, high specific thrust, high specific impulse, it is combining the advantages of the ATR and solid ramjet, and suitable for tactical missiles application meets potential requirements for boosting and cruising.

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Periodical:

Applied Mechanics and Materials (Volumes 152-154)

Pages:

204-209

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.152-154.204

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Online since:

January 2012

Authors:

Sa Yang, Guo Qiang He, Yang Liu, Jiang Li

Keywords:

Air Turbo Ramjet, Solid Propellant Ramjet, Turbocharged Solid Propellant Ramjet

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