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Engine Test

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Book cover Operation of a Cryogenic Rocket Engine

Part of the book series: Springer Aerospace Technology ((SAT,volume 2))

Abstract

An important character of a rocket engine and its components is the lifetime. Because we don’t have plenty of it. As well as the lifetime, the number of engine cycles (hot runs) is limited. Therefore the consumed lifetime and cycles performed are subjects of exact accounting in the engine and component logbooks. For this purpose, a precise definition of what counts as a test is necessary. Concerning the contractual aspects between the operator of the facility and the customer, we speak about a test as soon as the feed lines of the test facility are filled. For this step the test clearance is necessary which means the complete test preparation is successfully performed. Even in the case of abortion shortly after this step, from the contractual view the test is considered as performed.

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References

  1. S.A Durteste, Transient model of the VINCI cryogenic upper stage rocket engine, AIAA Joint Propulsion Conference, Cincinnati, 2007

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  2. J. Gastal, J.R.L. Barton, VULCAIN: A cryogenic engine for ARIANE 5, lecture series 1993-01 von Karman Institute for Fluid Dynamics

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  3. D.T. Harrje, F.H. Reardon, Liquid propellant rocket combustion instability NASA SP-194 National Aerospace and Space Administration, U.S.A, 1972

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  4. P. James,Technological readiness of the vinci expander engine, IAC International Astronautical Congress, Glasgow, 2008

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  5. G. Ordonneau, F. Lévy, Low frequency oscillation phenomena during VULCAIN shutdown transient, AIAA Joint Propulsion Conference, Salt Lake City, 2001

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Correspondence to Wolfgang Kitsche .

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© 2010 Springer-Verlag Berlin Heidelberg

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Kitsche, W. (2010). Engine Test. In: Operation of a Cryogenic Rocket Engine. Springer Aerospace Technology, vol 2. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-10565-4_4

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  • DOI: https://doi.org/10.1007/978-3-642-10565-4_4

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  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-10564-7

  • Online ISBN: 978-3-642-10565-4

  • eBook Packages: EngineeringEngineering (R0)

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