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An Overview of the NASA FAP Hypersonics Project Airbreathing Propulsion Research

Author
Auslender, A. H.
Published
October 19, 2009.
Physical Description
1 electronic document
Additional Creators
Thomas, Scott R. and Suder, Kenneth L.
Online Version

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Summary
The propulsion research portfolio of the National Aeronautics and Space Administration Fundamental Aeronautics Program Hypersonics Project encompasses a significant number of technical tasks that are aligned to achieve mastery and intellectual stewardship of the core competencies in the hypersonic-flight regime. An overall coordinated programmatic and technical effort has been structured to advance the state-of-the-art, via both experimental and analytical efforts. A subset of the entire hypersonics propulsion research portfolio is presented in this overview paper. To this end, two programmatic research disciplines are discussed; namely, (1) the Propulsion Discipline, including three associated research elements: the X-51A partnership, the HIFiRE-2 partnership, and the Durable Combustor Rig, and (2) the Turbine-Based Combine Cycle Discipline, including three associated research elements: the Combined Cycle Engine Large Scale Inlet Mode Transition Experiment, the small-scale Inlet Mode Transition Experiment, and the High-Mach Fan Rig.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 20090037583.
LF99-9121.
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference; 19-23 Oct. 2009; Bremen; Germany.
Terms of Use and Reproduction
No Copyright.
View MARC record | catkey: 15996426