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Author
Gann, R. G. | Braun, E. | Cleary, T. G. | Harris, R. H., Jr. | Horkay, F. | Linteris, G. T. | McKenna, G. B. | Nyden, M. R. | Peacock, R. D. | Ricker, R. E. | Stoudt, M. R. | Waldron, W. K.
Title
Agent/System Compatibility for Halon 1301 Aviation Replacement.
Coporate
National Institute of Standards and Technology, Gaithersburg, MD
Book or Conf
U.S. Environmental Protection Agency, Environment Canada and United National Environmental Program. International CFC and Halon Alternatives Conference, 1993. Stratospheric Ozone Protection for the 90's. October 20-22, 1993, Washington, DC, 753-760 p., 1993
Keywords
halons | ozone | halon 1301 | compatability | residues | storage stability | combustion products | corrosion | elastomers | exposure
Identifiers
environmental requirements
Abstract
This project has developed measurement methods and provided data for the appraisal of 12 USAF-specified candidate halon 1301 replacements for compatibility with flight systems, people, and the environment. The exposures of metals, elastomers and lubricants involve an initial temperature and pressure of 298 K (77 deg F) and 4.1 MPa (600 psi), with a final temperature of 422 K (300 deg F). These data and those from the companion project, "Agent Screening for Halon 1301 Aviation Replacement," will enable the selection by September 30, 1993 of 3 of the chemicals for full-scale testing by the Air Force. Longer-term testing will then be commenced to increase confidence in the preliminary results for materials compatibility. A final report will be delivered by September 30, 1995.