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Robust Rocket Engine ConceptThe potential for a revolutionary step in the durability of reusable rocket engines is made possible by the combination of several emerging technologies. The recent creation and analytical demonstration of life extending (or damage mitigating) control technology enables rapid rocket engine transients with minimum fatigue and creep damage. This technology has been further enhanced by the formulation of very simple but conservative continuum damage models. These new ideas when combined with recent advances in multidisciplinary optimization provide the potential for a large (revolutionary) step in reusable rocket engine durability. This concept has been named the robust rocket engine concept (RREC) and is the basic contribution of this paper. The concept also includes consideration of design innovations to minimize critical point damage.
Document ID
19950025700
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lorenzo, Carl F.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1995
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-TM-107010
E-9794
NAS 1.15:107010
Report Number: NASA-TM-107010
Report Number: E-9794
Report Number: NAS 1.15:107010
Accession Number
95N32121
Funding Number(s)
PROJECT: RTOP 505-62-50
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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