173. Weight Saving With Titanium
| Title | 173. Weight Saving With Titanium |
| Publication Type | Conference Paper |
| Paper Number | 0173 |
| Year of Publication | 1958 |
| Authors | Eshman, A. N. |
| Conference | 17th Annual Conference, Belmont Plaza Hotel, New York, New York, May 19-22 |
| Conference Location | New York, New York |
| Publisher | Society of Allied Weight Engineers, Inc. |
| Date Published | 5/19/58 |
| Abstract | Through research, the titanium industry has developed a new family of titanium alloys which offer potential weight saving to the aircraft Design Engineer. Three of these alloys are reviewed. MSM 2.5A1-16V possesses excellent formability and is heat treatable. MSM 821 is weldable and has high hot strength and creep resistance. MSM 185 is heat treatable to give the highest strength/weight ratio of any commercial materiel currently in use. |
| Pages | 11 |
| Key Words | 27. Weight Reduction - Materials |
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