NASA NTRS · 19930008102
STME nozzle thermal analysis
Abstract
The current summer project has the objective of carrying out a detailed thermal analysis of the Space Transportation Main Engine (STME) nozzle. The design and development of the STME nozzle has been undertaken by Pratt and Whitney in collaboration with NASA/MSFC and DoD. The nozzle design has adopted film/convective cooling techniques. The turbine exhaust has been utilized as the coolant in the nozzle cooling system.
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Das, Digendra K.. 1992-12-01. STME nozzle thermal analysis. https://ntrs.nasa.gov/citations/19930008102
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