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NASA NTRS · 19800028433

The 60-MW Shuttle Interaction Heating Facility

Abstract

An arc-heated wind-tunnel system described in the present paper will simulate aerodynamic heating in large-scale tests of the thermal protection system of the Shuttle Orbiter Vehicle during entry. The system provides for large-scale subsystem tests in high-enthalpy streams with boundary layer flows at high Reynolds numbers and for large test-body sizes in stagnation flows. The discussion covers the design concept of the arc-jet systems, the extensive hardware developments of the arc heater to provide reliable operation, and verification and performance measurements of the system's operating envelopes.

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BibTeXRIS

W Winovich, W C A Carlson. 1979-01-01. The 60-MW Shuttle Interaction Heating Facility. https://ntrs.nasa.gov/citations/19800028433

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