An interface design for a shock-tube system
dc.contributor.author | Beevis, D. | |
dc.contributor.author | Leamon, T. B. | |
dc.contributor.author | Lovesey, E. J. | |
dc.contributor.author | Neale, J. G. | |
dc.contributor.author | Strank, R. H. D. | |
dc.date.accessioned | 2016-10-28T14:31:41Z | |
dc.date.available | 2016-10-28T14:31:41Z | |
dc.date.issued | 1964-08 | |
dc.description.abstract | A linear display of lights and a mimic diagram arrangement of switches are suggested for the proposed high pressure shock tube control panel to enable the operator to follow a safe and reliable operating procedure. | en_UK |
dc.identifier.uri | http://dspace.lib.cranfield.ac.uk/handle/1826/10908 | |
dc.language.iso | en | en_UK |
dc.publisher | College of Aeronautics | en_UK |
dc.relation.ispartofseries | CoA/M/M&P-44 | en_UK |
dc.relation.ispartofseries | 44 | en_UK |
dc.title | An interface design for a shock-tube system | en_UK |
dc.type | Report | en_UK |