NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Low thrust rocket test facilityA low thrust chemical rocket test facility has recently become operational at the NASA-Lewis. The new facility is used to conduct both long duration and performance tests at altitude over a thruster's operating envelope using hydrogen and oxygen gas for propellants. The facility provides experimental support for a broad range of objectives, including fundamental modeling of fluids and combustion phenomena, the evaluation of thruster components, and life testing of full rocket designs. The major mechanical and electrical systems are described along with aspects of the various optical diagnostics available in the test cell. The electrical and mechanical systems are designed for low down time between tests and low staffing requirements for test operations. Initial results are also presented which illustrate the various capabilities of the cell.
Document ID
19900060170
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Arrington, Lynn A.
(NASA Lewis Research Center; Sverdrup Technology, Inc. Brook Park, OH, United States)
Schneider, Steven J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 14, 2013
Publication Date
July 1, 1990
Subject Category
Ground Support Systems And Facilities (Space)
Report/Patent Number
AIAA PAPER 90-2503
Report Number: AIAA PAPER 90-2503
Accession Number
90A47225
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available