<div class="description">
<dl><dd>Thesis advisor(s): Garth V. Hobson</dd>
<dd>"December 1993."</dd>
<dd>Thesis (M.S. in Astronautical Engineering) Naval Postgraduate School, December 1993</dd>
<dd>Includes bibliographical references</dd>
<dd>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 &amp; 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. Turbine test rig, Alternate turbopump development model, SSME turbopump turbine</dd>
<dd>Mode of access: World Wide Web</dd>
<dd>System requirements: Adobe Acrobat Reader</dd>
<dd>US Navy (USN) author</dd></dl><br>Subjects:</div>
<div class="fn value">
Studevan, Colin C.</div>
Internet Archive identifier