Hyper-X Mach 10 Engine Flowpath Development: Fifth Entry Test Conditions and Methodology

Topics:
Aerospace and Defense
Tags:
Body,
Human Resources,
Performance Management,
Workforce Management
Source:
American Institute of Aeronautics and Astronautics

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Overview: A series of Hyper-X Mach 10 flow path ground tests are underway to obtain engine performance and operation data to confirm and refine the flow path design methods. The model used is a full-scale height, partial-width replica of the Hyper-X Research Vehicle propulsive flow path with truncated fore body and aft body. This paper presents a review of the test conditions, model calibrations, and a description of steady flow confirmation. The test series included runs using hydrogen fuel, and a silane-in-hydrogen fuel mixture.

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Format: PDF | Size: 342KB | Date: Jun 2001 | Pages: 14

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