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1

Laverty, Danny Anthony. Investigation of the thermo-structural response of axially loaded concrete masonry walls using a model test methodology. The Author], 2002.

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2

United States. National Aeronautics and Space Administration., ed. Monoball energy transfer: Test report. University of Alabama, 1986.

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3

United States. National Aeronautics and Space Administration. Office of the Chief Engineer. Evaluation of the NASA arc jet capabilities to support mission requirements. National Aeronautics and Space Administration, Office of the Chief Engineer, 2010.

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4

Smith, David R. Interlaboratory comparison of the guarded horizontal pipe-test apparatus: Precision of ASTM standard test method C-335 applied to mineral-fiber pipe insulation. U.S. Dept. of Commerce, National Institute of Standards and Technology, 1989.

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5

United States. National Aeronautics and Space Administration., ed. QM-8 field joint protection system final report. Morton Thiokol, Inc., Space Division, 1989.

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6

United States. National Aeronautics and Space Administration., ed. QM-8 field joint protection system final report. Morton Thiokol, Inc., Space Division, 1989.

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7

United States. National Aeronautics and Space Administration., ed. QM-8 field joint protection system final report. Morton Thiokol, Inc., Space Division, 1989.

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8

Cooling Tower Institute (U.S.). CTI code tower standard specifications: Acceptance test code for water cooling towers. Cooling Tower Institute, 2000.

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9

Keyser, Matt. NREL battery thermal and life test facility. National Renewable Energy Laboratory, 2011.

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10

IEEE Power Engineering Society. Transformers Committee., Institute of Electrical and Electronics Engineers., IEEE Xplore (Online service), and Institute of Electrical and Electronics Engineers., eds. IEEE standard test procedure for thermal evaluation of liquid-immersed distribution and power transformers. The Institute of Electrical and Electronics Engineers, 1999.

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11

American Society of Heating and Air-Conditioning Engineers. and American National Standards Institute, eds. Calorimeter test methods for mass flow measurements of volatile refrigerants. American Society of Heating, Refrigerating and Air-Conditioning Engineers, 2006.

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12

Rosa, Maria I. De. Predicting materials' ease of combustion: Development of a simple test method. U.S. Dept. of the Interior, Bureau of Mines, 1992.

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13

A, Scheiman David, and United States. National Aeronautics and Space Administration., eds. Thermal cycling of Mir Cooperative Solar Array (MCSA) test panels. National Aeronautics and Space Administration, 1997.

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14

Wilkinson, C. High temperature cyclic behaviour of aerospace materials: room temperature validation tests of Ti-6Al-4V. AGARD, 1994.

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15

Wong, Chung-Nin Channy. HECTR analyses of the Nevada Test Site (NTS) premixed combustion experiments. Division of Systems Research, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1988.

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16

S, Greenberg H., Johnson S. E, and United States. National Aeronautics and Space Administration., eds. Reusable LH2 tank technology demonstration through ground test. National Aeronautics and Space Administration, 1995.

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17

United States. National Aeronautics and Space Administration., ed. Test plans, lightweight durable TPS tasks, 1,2,4,5, and 6. Rockwell Aerospace, Space Systems Division, 1994.

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18

United States. National Aeronautics and Space Administration. and Lewis Research Center, eds. Vibration and thermal vacuum qualification test results for a low-voltage tungsten-halogen light. National Aeronautics and Space Administration, 1991.

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19

A, Miller Robert, and Lewis Research Center, eds. Investigation of thermal high cycle and low cycle fatigue mechanisms of thick thermal barrier coatings. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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20

A, Miller Robert, and Lewis Research Center, eds. Investigation of thermal high cycle and low cycle fatigue mechanisms of thick thermal barrier coatings. National Aeronautics and Space Administration, Lewis Research Center, 1998.

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21

Alexander, Dennis. 2 kWe Solar Dynamic Ground Test Demonstration Project. National Aeronautics and Space Administration, 1997.

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22

Alexander, Dennis. 2 kWe Solar Dynamic Ground Test Demonstration Project. National Aeronautics and Space Administration, 1997.

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23

Alexander, Dennis. 2 kWe Solar Dynamic Ground Test Demonstration Project. National Aeronautics and Space Administration, 1997.

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24

Stecher, Joseph L. 15th Space Simulation Conference: Support the highway to space through testing : proceedings of a symposium sponsored by the National Aeronautics and Space Administration, Institute of Environmental Sciences, the American Institute for Aeronautics and Astronautics, and the American Society for Testing and Materials and held at the Williamsburg Hilton and National Conference Center, Williamsburg, Virginia, October 31 to November 3, 1988. Edited by Goddard Space Flight Center. Goddard Space Flight Center, 1989.

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25

G, Fox Alan. The influence of TIG welding thermal cycles on HSLA-100 steel plate. Naval Postgraduate School, 1993.

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26

Issa, Mohsen A. Evaluation of Washington Hydraulic Fracture Test (SHRP) for D-cracking aggregate: Final report. Illinois Transportation Research Center, Illinois Dept. of Transportation, 1999.

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27

T, Rothfuchs, Gesellschaft für Strahlen- und Umweltforschung., and Battelle Memorial Institute. Office of Nuclear Waste Isolation., eds. Brine migration test: Asse Salt Mine, Federal Republic of Germany : final report. Gesellschaft für Strahlen- und Umweltforschung, 1988.

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28

Bragova, Arina. Tests on the Latin language. Publishing Center RIOR, 2024. http://dx.doi.org/10.29039/02139-2.

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The manual consists of 34 tests on the Latin language, which test linguistic terminology, phonetics, vocabulary, grammar and word formation of the Latin language of the classical period. The tests are grouped into sections: phonetics, morphology, syntax, and case functions. Each test consists of two parts: the first part (the first ten questions) tests knowledge of theory, the second part (the second ten questions) contains practical tasks in the Latin language. The tests correspond to the federal state educational standard in the discipline “Ancient Languages and Cultures” for training areas
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29

Mehos, Mark S. Acceptance performance test guideline for utility scale parabolic trough and other CSP solar thermal systems: Preprint. National Renewable Energy Laboratory, 2011.

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30

Mital, Subodh K. Fiber pushout test: A three-dimensional finite element computational simulation. NASA, 1990.

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31

DeAngelis, V. Michael. Techniques for hot structures testing. NASA Ames Research Center, Dryden Flight Research Facility, 1990.

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32

DeAngelis, V. Michael. Techniques for hot structures testing. NASA Ames Research Center, Dryden Flight Research Facility, 1990.

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33

(Firm), Aerojet, and United States. National Aeronautics and Space Administration., eds. Integrated Advanced Microwave Sounding Unit-A (AMSU-A), performance verification report, METSAT Phase Locked Oscillator assembly, P/N 1348360-1, S/N's F07 and F08: Contract no. NAS 5-32314. National Aeronautics and Space Administration, 1998.

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34

M, Michal Gary, and United States. National Aeronautics and Space Administration., eds. Mechanical and thermal properties of two Cu-Cr-Nb alloys and NARloy-Z. National Aeronautics and Space Administration, 1996.

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35

United States. National Aeronautics and Space Administration., ed. Solar thermal propulsion optical figure measuring and rocket engine testing: Final technical report, NASA/MSFC, contract number NAS8-38609 DO 147. University of Alabama in Huntsville, Propulsion Research Center, 1997.

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36

(Firm), Aerojet, and United States. National Aeronautics and Space Administration., eds. Integrated Advanced Microwave Sounding Unit-A (AMSU-A), performance verification report, METSAT Phase Locked Oscillator assembly, P/N 1348360-1, S/N's F07 and F08: Contract no. NAS 5-32314. National Aeronautics and Space Administration, 1998.

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37

United States. National Aeronautics and Space Administration., ed. Solar thermal propulsion optical figure measuring and rocket engine testing: Final technical report, NASA/MSFC, contract number NAS8-38609 DO 147. University of Alabama in Huntsville, Propulsion Research Center, 1997.

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38

United States. National Aeronautics and Space Administration., ed. Microcracking in composite laminates under thermal and mechanical loading. National Aeronautics and Space Administration, 1995.

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39

L, Frost C., Engel Carl D, and George C. Marshall Space Flight Center., eds. SRB ascent aerodynamic heating design criteria reduction study: Final report. Renault Vehicles Industriels, 1989.

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40

L, Stecher Joseph, and Goddard Space Flight Center, eds. 20th Space Simulation Conference: The Changing Testing Paradigm. National Aeronautics and Space Administration, Goddard Space Flight Center, 1998.

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41

Shaltens, Richard K. Initial results from the solar dynamic (SD) ground test demonstration (GTD) project at NASA Lewis. National Aeronautics and Space Administration, 1995.

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42

Shaltens, Richard K. Initial results from the solar dynamic (SD) ground test demonstration (GTD) project at NASA Lewis. National Aeronautics and Space Administration, 1995.

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43

M, Viens, Wang L, and Goddard Space Flight Center, eds. Evaluation of engineering properties of Al-Li alloy X2096-T8A3 extrusion products. National Aeronautics and Space Administration, Goddard Space Flight Center, 1999.

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44

M, Viens, Wang L, and Goddard Space Flight Center, eds. Evaluation of engineering properties of Al-Li alloy X2096-T8A3 extrusion products. National Aeronautics and Space Administration, Goddard Space Flight Center, 1999.

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45

L, Perry Jimmy, and George C. Marshall Space Flight Center., eds. International Space Station Alpha trace contaminant control subassembly life test final report. National Aeronautics and Space Administration, Marshall Space Flight Center, 1995.

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46

Purnell, Hopson, Mau Johnny C, and Langley Research Center, eds. Assembly and integration of superconductive measurement circuits for a spaceflight experiment. National Aeronautics and Space Administration, Langley Research Center, 1998.

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47

George C. Marshall Space Flight Center., ed. Permeability testing of composite material and adhesive bonds for the DC-XA composite feedline program. National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1995.

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48

D, Mellott Kenneth, and United States. National Aeronautics and Space Administration., eds. Space Station Freedom solar array panels plasma interaction test facility. NASA, 1990.

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49

Martin, Donald F. Space Station Freedom solar array panels plasma interaction test facility. NASA, 1990.

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50

J, Barrow Betty, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Thermal-fatigue and oxidation resistance of cobalt-modified Udimet 700 alloy. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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