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Low thrust rocket test facility
Author(s) -
Lynn Arrington,
Steven P. Schneider
Publication year - 1990
Publication title -
24th joint propulsion conference
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.1990-2503
Subject(s) - test (biology) , aeronautics , rocket (weapon) , thrust , aerospace engineering , computer science , engineering , geology , paleontology
A 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.

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