Flammability, odor, and offgassing requirements and test procedures for materials in environments that support combustion
National Aeronautics and Space Administration, Office of Space Transportation Systems, 1981 - Technology & Engineering
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4l0 Details of Striker Sample Cup Sample 458
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approved assembled article assembly burning calibration candidate materials center program office CENTRAL CONNECTOR cleaning coating cognizant NASA center combustion configuration tests crew bay CRITERIA FOR ACCEPTABILITY described in paragraph determined Dewar flask electrical ELECTRICAL CONNECTOR ELECTRICAL OVERLOAD environment evaluated exposed fire point flame propagation rate flammability FLAMMABILITY TEST flash point form similar gage Gas Chromatograph ignition source IMPACT TEST inch insulation leak liters materials applications Maximum Allowable Concentration maximum use pressure MECHANICAL IMPACT meet the requirements minimum minutes nitrogen offgassed products oxygen paragraph 208 plummet pressure and temperature psia quantity requirements of Test sample cup sample holder sample material self-extinguishing similar to Figure spacecraft spacecraft atmosphere spark specified stainless steel striker pins subparagraph surface Teflon test atmosphere test chamber TEST CONDITIONS test equipment TEST Materials test pressure TEST PROCEDURE test specimen test temperature testing agency thermocouples Type vacuum Verify wire