نتائج البحث

Testing of Heat Flux Sensors at Cryogenic Temperatures

• Authors : Johnson, W. L; Balasubramaniam, R; Westra, K

Subjects: Fluid Mechanics And Thermodynamics

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Laboratory-Based Thermal Shock Investigation of Heat Flux Sensors for the Mars 2020 Backshell

• Authors : Miller, R. A; Swanson, G. T; Santos, J. A

Subjects: Spacecraft Design, Testing And Performance

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Laboratory-Based Thermal Shock Investigation of Heat Flux Sensors for the Mars 2020 Backshell

• Authors : Miller, R. A; Swanson, G. T; Santos, J. A

Subjects: Spacecraft Design, Testing And Performance; Instrumentation And Photography

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Thin Film Heat Flux Sensors: Design and Methodology

• Authors : Fralick, Gustave C; Wrbanek, John D

Subjects: Fluid Mechanics And Thermodynamics

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Thin-Film Resistance Heat-Flux Sensors

• Authors : Fralick, Gustave C; Wrbanek, John D; Blaha, Charles A

Subjects: Instrumentation And Photography

• Source: NASA Tech Briefs, July 2005.

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Diamond thin film temperature and heat-flux sensors

• Authors : Aslam, M; Yang, G. S; Masood, A

Subjects: Solid-State Physics

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Novel thin-film heat flux sensors

• Authors : Bhatt, Hemanshu; Zeller, Mary; Will, Herbert

Subjects: Instrumentation And Photography

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Fabrication of Thin Film Heat Flux Sensors

• Authors : Will, Herbert A

Subjects: Instrumentation And Photography

• Source: NASA. Langley Research Center, The 1992 NASA Langley Measurement Technology Conference: Measurement Technology for Aerospace Applications in High-Temperature Environments.

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Fabrication of thin film heat flux sensors

• Authors : Will, Herbert

Subjects: Instrumentation And Photography

• Source: In: Annual Health Monitoring Conference for Space Propulsion Systems, 3rd, Cincinnati, OH, Nov. 13, 14, 1991, Proceedings (A93-16401 04-20).

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Numerical study of the effects of boundary conditions on the measurement and calibration of gardon type heat flux sensors

• Authors : Krane, M; Dybbs, A

Subjects: Instrumentation And Photography

• Source: NASA. Lewis Research Center Structural Integrity and Durability of Reusable Space Propulsion Systems.

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