NASA Technical Reports Server (NTRS) : Eroding pdf

NASA Technical Reports Server (NTRS) : Eroding

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Eroding potentiometers have been devised for measuring the time-dependent positions of char fronts advancing through layers of insulating material subject to intense heating from one side. In the original application, the material layers of interest are thermal insulators in rocket motors and the heat comes from firing of the motors, but the principle of operation is equally applicable to other insulating materials subject to intense heating (e.g., ablative fire-retardant materials). Measuring the thickness decrement of propellant (in hybrid motors in particular) is another possible application of this transducer. Telemetry informs mission control of the propellant left after each burn. An eroding potentiometer could be characterized, more precisely, as an eroding two-wire resistor. It includes a twisted pair of thin, insulated wires oriented along the thickness of, and embedded in, the layer of thermal-insulation material to be tested (see figure). The electrical insulation material on the wires should be one for which the charring temperature is about the same as (or perhaps slightly less than) that of the thermal- insulation material to be tested.

In the original rocket-motor application, the wires have a diameter of 0.003 in. (.0.08 mm), are made of manganin, and are coated with polyimide for electrical insulation. Outside the thermal insulation on the cold side, the wire leads are connected to a Wheatstone bridge circuit for measurement of electrical resistance change

• Creator/s: NASA Technical Reports Server (NTRS
• Date: 2/1/2003
• Year: 2003
• Book Topics/Themes: NASA Technical Reports Server (NTRS), CHARRING, TRANSDUCERS, ABLATIVE MATERIALS, ELECTRICAL RESISTANCE, INSULATORS, THERMAL INSULATION, TIME DEPENDENCE, INSULATION, POLYIMIDES, PROPELLANTS, ROCKET ENGINES, Eggett, Mark, Shipley, John L., Godfrey, Alan L., Johnson, Lloyd T., Johnson, Mont, Bryner, Boyd D., McWhorter, Bruce

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