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STME nozzle thermal analysisThe 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.
Document ID
19930008102
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Das, Digendra K. (State Univ. of New York Stony Brook, NY, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1992
Publication Information
Publication: Alabama Univ., 1992 NASA(ASEE Summer Faculty Fellowship Program
Subject Category
Spacecraft Propulsion And Power
Accession Number
93N17291
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19930008090Collected Works1992 NASA/ASEE Summer Faculty Fellowship Program
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