Dimensional changes resulting from the heat treatment of EN 30B and Nimar 125

dc.contributor.author	Noble, C. F.
dc.date.accessioned	2017-10-11T08:23:55Z
dc.date.available	2017-10-11T08:23:55Z
dc.date.issued	1966-12
dc.identifier.uri	http://dspace.lib.cranfield.ac.uk/handle/1826/12610
dc.description.abstract	Three components have been manufactured in both EN 30B and N1MAR 125. Dimensional changes following heat treatment have been recorded and, while the sample is only small, the report serves to illustrate the potential benefits which arise from the use of a maraging steel. NIMAR 125 is shown to have reasonably predictable dimensional characteristics and thus indicates the feasibility of completing all machining operations prior to heat treatment.	en_UK
dc.language.iso	en	en_UK
dc.publisher	College of Aeronautics	en_UK
dc.relation.ispartofseries	CoA/N/M&P-15	en_UK
dc.relation.ispartofseries	15	en_UK
dc.title	Dimensional changes resulting from the heat treatment of EN 30B and Nimar 125	en_UK
dc.type	Report	en_UK