NASA-STD-(I)-6001A, NASA TECHNICAL STANDARD (INTERIM), FLAMMABILITY, OFFGASSING, AND COMPATIBILITY REQUIREMENTS AND TEST PROCEDURES (21 APR 2009)

NASA-STD-(I)-6001A, NASA TECHNICAL STANDARD (INTERIM), FLAMMABILITY, OFFGASSING, AND COMPATIBILITY REQUIREMENTS AND TEST PROCEDURES (21 APR 2009)., This Interim Technical Standard is published by the National Aeronautics and Space Administration (NASA) to provide uniform engineering and technical requirements for processes, procedures, practices, and methods to meet urgent program and project technical needs. This interim standard has the consensus of the developing Technical Working Group but does not have Agencywide concurrence required for a NASA technical standard. This interim standard may be cited in contract, program, and other Agency documents as a technical requirement. This document establishes requirements for evaluation, testing, and selection of materials that are intended for use in space vehicles, associated Ground Support Equipment (GSE), and facilities used during assembly, test, and flight operations. Included are requirements, criteria, and test methods for evaluating the flammability, offgassing, and compatibility of materials. Provisions of this standard will be included, as applicable, in all future contracts and programs involving space vehicles, payloads, and associated support equipment. NASA-STD-6001 was previously published as NHB 8060.1, Flammability, Odor, Offgassing, and Compatibility Requirements and Test Procedures for Materials in Environments that Support Combustion.