Metallic Materials Properties Development and Standardization
The military handbook Mil-Hdbk-5J-Not-1 is now canceled and replaced by a "civil" manual. As these two documents are very similar, the newer manual is referenced as a military document.
Document ID:Mil-Hdbk-5J-Not-1
Overview
| Title: |
Metallic materials and elements for aerospace vehicle structures (see notice 1 for additional information) |
| Scope: |
This Handbook is primarily intended to provide a source of design mechanical and physical properties, and joint allowables. Material property and joint data obtained from tests by material and fastener producers, government agencies, and members of the airframe industry are submitted to Mil-Hdbk-5 for review and analysis. Results of these analyses are submitted to the membership during semi-annual coordination meetings for approval and, when approved, published in this Handbook. |
| Document Status: |
Canceled |
Doc Date: |
05-MAY-2004 |
QPL⁄QML: |
None |
| FSC⁄Area: |
1560 |
Dist Stmt: |
A |
|
|
| Doc Category: |
Military Handbooks |
Replaced by:
Metallic Materials Properties Development and Standardization (MMPDS). - Rept. for 1 Jan 02-31 Dec 02.
Battelle Memorial Inst., Columbus, OH.; William J. Hughes Technical Center, Atlantic City, NJ.; Federal Aviation Administration, Washington, DC. Office of Aviation Research.
Product Type: Technical report
NTIS Order Number: PB2003-106632
$116.50-Microfiche $223.50-Paper
Page Count: 1732 pages
Date: Jan 2003
Author: R. C. Rice, J. L. Jackson, J. Bakuckas, S. Thompson
The Metallic Material Properties Development and Standardization (MMPDS) Handbook is the replacement document for MILHDBK- 5. It is recognized internationally as a reliable source of aircraft materials data for aerospace materials selection and analysis. Consistent and reliable methods are used to collect, analyze, and present statistically based material and fastener allowable properties. The Handbook is the only publicly available source in the U.S. for material allowables that the Federal Avaiation Administration generally accepts for compliance with Federal Aviation Regulations (FAR) for material strength properties and design values for aircraft certification and continued airworthiness. Moreover, it is the only publicly available source worldwide for fastener joint allowables that comply with the FARs. This edition, MMPDS-01, incorporates the additions and changes to aircraft metallic material design properties and analysis guidelines approved at the 1st and 2nd MMPDS government⁄industry coordination meetings. This year, 2003, marks the first year of publication of the MMPDS Handbook and the final year of publication of Mil-Hdbk-5. For this year only, MMPDS-01 and Mil-Hdbk-5J will be technically equivalent. In the spring of 2004, when the 1st Change Notice of MMPDS-01 is published, Mil-Hdbk-5 will be designated noncurrent and MMPDS will become the only governmentrecognized source in the U.S. of published design allowable properties for metallic commercial and military aircraft structures and mechanically fastened joints. In this way, the 65-year legacy of Mil-Hdbk-5, and its predecessor ANC-5, will be maintained.
Notes
Product reproduced from digital image.
Prepared in cooperation with William J. Hughes Technical Center, Atlantic City, NJ. Sponsored by Federal Aviation Administration, Washington, DC. Office of Aviation Research.
Report Number: N⁄A; DOT⁄FAA⁄AR-MMPDS-01
Contract Number: N⁄A
Project Number: N⁄A
Task Number: N⁄A
NTIS announcement issue: 0321
"N⁄A" indicates no data is available for this field.
