Integral Rocket-ramjet Component Evaluation Test Program (U). PDF Download
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Author: C. E. Franklin
Publisher:
ISBN:
Category : Combustion
Languages : en
Pages : 174
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Book Description
Author: C. E. Franklin
Publisher:
ISBN:
Category : Combustion
Languages : en
Pages : 174
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Book Description
Author: C. E. Franklin
Publisher:
ISBN:
Category : Combustion
Languages : en
Pages : 642
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Author: Hisahiro Nakayama
Publisher:
ISBN:
Category :
Languages : en
Pages : 14
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Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 98
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 702
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Author: R. R. Conley
Publisher:
ISBN:
Category : Air-to-air missiles
Languages : en
Pages : 208
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Author:
Publisher:
ISBN:
Category : Armed Forces
Languages : en
Pages : 168
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Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 436
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 40
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Book Description
This report describes the main accomplishments of a collaborative Canadian-Dutch project known as the Integral Rocket Ramjet Demonstration Program (IRRDP) to investigate the key technologies of air-breathing missile propulsion through the design, fabrication, & testing of a solid fuel ducted rocket engine with an integral booster for a medium-range air-launched missile. It begins by discussing the requirements for an integral rocket ramjet engine, then reviews activities related to the development of a missile design tool & performance prediction tool, computational fluid dynamics evaluation of the intake & port covers, development of a new solid propellant for a gas generator used in ducted rocket propulsion, modelling of the ramjet combustor in a water tunnel, combustion tests, modelling & propellant development for the nozzle-less booster, and the final design.
Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 552
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