Design of a cold-flow test facility for the high-pressure fuel turbopump turbine of the space-shuttle main engine

Design of a cold-flow test facility for the high-pressure fuel turbopump turbine of the space-shuttle main engine

Approved for public release; distribution is unlimited === The design and installation at the Naval Postgraduate School of a cold-flow test facility for the turbine of the high-pressure fuel turbopump of the Space Shuttle Main Engine, is reported. The specific article to be tested is the 'Alter...

Full description

Bibliographic Details
Main Author: Studevan, Colin C.
Other Authors: Hobson, Garth V.
Language:en_US
Published: Monterey, California. Naval Postgraduate School 2012
Online Access:http://hdl.handle.net/10945/19733
id ndltd-nps.edu-oai-calhoun.nps.edu-10945-19733
record_format oai_dc
spelling ndltd-nps.edu-oai-calhoun.nps.edu-10945-197332015-08-15T15:59:35Z Design of a cold-flow test facility for the high-pressure fuel turbopump turbine of the space-shuttle main engine Studevan, Colin C. Hobson, Garth V. Shreeve, Raymond P. Naval Postgraduate School (U.S.) Department of Aeronautical Engineering Approved for public release; distribution is unlimited The design and installation at the Naval Postgraduate School of a cold-flow test facility for the turbine of the high-pressure fuel turbopump of the Space Shuttle Main Engine, is reported. The specific article to be tested is the 'Alternate Development Model' designed and manufactured by Pratt & Whitney. The design of individual components is documented. The installation of the facility subsystem is described in detail. A preliminary estimation of turbine performance is made. 2012-11-19T23:58:11Z 2012-11-19T23:58:11Z 1993-12 Thesis http://hdl.handle.net/10945/19733 en_US This publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. As such, it is in the public domain, and under the provisions of Title 17, United States Code, Section 105, it may not be copyrighted. Monterey, California. Naval Postgraduate School
collection NDLTD
language en_US
sources NDLTD
description Approved for public release; distribution is unlimited === The design and installation at the Naval Postgraduate School of a cold-flow test facility for the turbine of the high-pressure fuel turbopump of the Space Shuttle Main Engine, is reported. The specific article to be tested is the 'Alternate Development Model' designed and manufactured by Pratt & Whitney. The design of individual components is documented. The installation of the facility subsystem is described in detail. A preliminary estimation of turbine performance is made.
author2 Hobson, Garth V.
author_facet Hobson, Garth V.
Studevan, Colin C.
author Studevan, Colin C.
spellingShingle Studevan, Colin C.
Design of a cold-flow test facility for the high-pressure fuel turbopump turbine of the space-shuttle main engine
author_sort Studevan, Colin C.
title Design of a cold-flow test facility for the high-pressure fuel turbopump turbine of the space-shuttle main engine
title_short Design of a cold-flow test facility for the high-pressure fuel turbopump turbine of the space-shuttle main engine
title_full Design of a cold-flow test facility for the high-pressure fuel turbopump turbine of the space-shuttle main engine
title_fullStr Design of a cold-flow test facility for the high-pressure fuel turbopump turbine of the space-shuttle main engine
title_full_unstemmed Design of a cold-flow test facility for the high-pressure fuel turbopump turbine of the space-shuttle main engine
title_sort design of a cold-flow test facility for the high-pressure fuel turbopump turbine of the space-shuttle main engine
publisher Monterey, California. Naval Postgraduate School
publishDate 2012
url http://hdl.handle.net/10945/19733
work_keys_str_mv AT studevancolinc designofacoldflowtestfacilityforthehighpressurefuelturbopumpturbineofthespaceshuttlemainengine
_version_ 1716817086614863872

Similar Items