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H6 - Federal Item Name Directory
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22411
NOZZLE,EXHAUST,ROCKET MOTOR
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FIIG: A23900
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Entry Date: Apr-01-1974
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Concept:
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Status: A
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Applicability: A
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Type: 0
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Definition: An item designed with a constricting throat section and a divergent section. The constricting throat section compresses the propellant gases and maintains the pressure within the thrust chamber of the rocket motor by limiting the flow of gases. The divergent section controls the expansion of the gases causing increased thrust.
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Basic INC: 70686
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Basic Name: NOZZLE
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Description: 1. A short tubular item with a taper or a constricting section, of various configurations, with a fixed or adjustable outlet opening. It is used to disperse, direct and control the flow of pressurized substances.
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Corresponding NIINs: 32
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