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oaioai:casi.ntrs.nasa.gov:19790022112

Handbook of recommended practices for the determination of liquid monopropellant rocket engine performance

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1979
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Abstract

The design, installation, and operation of systems to be used for directly measuring quantities of fundamental importance to the determination of monopropellant thruster performance is described. Areas covered include: (1) force and impulse measurement; (2) propellant mass usage and flow measurement; (3) pressure measurement; (4) temperature measurement; (5) exhaust gas composition measurement; and (6) data reduction and performance determination

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This paper was published in NASA Technical Reports Server.

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