Specification for aircraft material. 1½ per cent nickel-chromium-molybdenum steel (65/75 tonf/sq in: limiting ruling section 2½ in). (31st January 1964)

• Record Type: Book
• Authors: British Standards Institution,
• Publisher Details: London : British Standards Institution
• Publication Date: 1964
• Extent: 1 online resource (3 pages)
• Subjects: 602.1841; Mechanical properties of materials; Heat treatment; Designations; Steels; Chemical composition; Molybdenum steels; Bars (materials); Aircraft components; Air transport engineering; Hardness; Tensile strength; Nickel steels; Low-alloy steels; Chromium steels; Billets; Forgings; Alloy steels
• Languages: English
• ISSNs: 0012-4435
• Access Rights: Legal Deposit; Only available on premises controlled by the deposit library and to one user at any one time; The Legal Deposit Libraries (Non-Print Works) Regulations (UK).
• Access Usage: Restricted: Printing from this resource is governed by The Legal Deposit Libraries (Non-Print Works) Regulations (UK) and UK copyright law currently in force.