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Title: Liquid hydrogen turbopump ALS advanced development program. Volume 1: Hot fire unit

Abstract

The interface criteria for the Turbopump Test article (TPA) and the Component Test Facility located at NASA, Stennis Space Center is defined by this interface Control Document (ICD). TPA ICD Volume 2 is submitted for the Cold Gas Drive Turbopump Test Article, which is generally similar but incorporates certain changes, particularly in fluid requirements and in instrumentation needs. For the purposes of this ICD, the test article consists of the Hot Fire Drive Turbopump mounted on its test cart, readied for installation in the component test facility. It should be emphasized that the LH2 turbopump program is still in its early concept design phase. Design of the turbopump, test cart, and spools are subject to revisions until successful conclusion of the Detail Design Review (DDR).

Authors:
Publication Date:
Research Org.:
Aerojet-General Corp., Sacramento, CA (United States)
OSTI Identifier:
5199536
Report Number(s):
N-91-27539; NASA-CR-187035; NAS-1.26:187035
CNN: NAS8-37593
Resource Type:
Technical Report
Country of Publication:
United States
Language:
English
Subject:
71 CLASSICAL AND QUANTUM MECHANICS, GENERAL PHYSICS; PUMP TURBINES; DESIGN; TEST FACILITIES; HYDROGEN; MEASURING INSTRUMENTS; ROCKET ENGINES; ELEMENTS; ENGINES; HYDRAULIC TURBINES; MACHINERY; NONMETALS; TURBINES; TURBOMACHINERY; 420201* - Engineering- Cryogenic Equipment & Devices

Citation Formats

Lindley, B. Liquid hydrogen turbopump ALS advanced development program. Volume 1: Hot fire unit. United States: N. p., 1990. Web.
Lindley, B. Liquid hydrogen turbopump ALS advanced development program. Volume 1: Hot fire unit. United States.
Lindley, B. 1990. "Liquid hydrogen turbopump ALS advanced development program. Volume 1: Hot fire unit". United States.
@article{osti_5199536,
title = {Liquid hydrogen turbopump ALS advanced development program. Volume 1: Hot fire unit},
author = {Lindley, B},
abstractNote = {The interface criteria for the Turbopump Test article (TPA) and the Component Test Facility located at NASA, Stennis Space Center is defined by this interface Control Document (ICD). TPA ICD Volume 2 is submitted for the Cold Gas Drive Turbopump Test Article, which is generally similar but incorporates certain changes, particularly in fluid requirements and in instrumentation needs. For the purposes of this ICD, the test article consists of the Hot Fire Drive Turbopump mounted on its test cart, readied for installation in the component test facility. It should be emphasized that the LH2 turbopump program is still in its early concept design phase. Design of the turbopump, test cart, and spools are subject to revisions until successful conclusion of the Detail Design Review (DDR).},
doi = {},
url = {https://www.osti.gov/biblio/5199536}, journal = {},
number = ,
volume = ,
place = {United States},
year = {Mon Oct 01 00:00:00 EDT 1990},
month = {Mon Oct 01 00:00:00 EDT 1990}
}

Technical Report:
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