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MODUK - DEF STAN 00-970: V2 P4

Detail Design and Strength of Materials

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Organization: MODUK
Publication Date: 10 March 1998
Status: active
Page Count: 196
scope:

In the detailed design of the Rotor craft, the variety of materials and parts shall be kept to a minimum consistent with structural efficiency and without unduly sacrificing structure weight. The design of parts and fittings shall be such as to facilitate their manufacture in quantity.

Components and items of equipment shall have at least the same factor as the main structure in all the appropriate stressing cases. Local loads at parts of attachment to the main structure shall be carefully considered to ensure that the main structure is not unduly weakened thereby

Document History

DEF STAN 00-970: V2 P4
March 10, 1998
Detail Design and Strength of Materials
In the detailed design of the Rotor craft, the variety of materials and parts shall be kept to a minimum consistent with structural efficiency and without unduly sacrificing structure weight. The...
February 1, 1994
Design and Airworthiness Requirements for Service Aircraft Volume 2 - Rotorcraft Book 2 (Parts 4 to 6)
A description is not available for this item.
February 1, 1992
Design and Airworthiness Requirements for Service Aircraft Volume 2 - Rotorcraft Book 2 (Parts 4 to 6) Part 4: Detail Design and Strength of Materials
GENERAL In the detailed design of the rotorcraft, the variety of materials and parts shall be kept to a minimum consistent with structural efficiency and without unduly sacrificing structure weight....
December 1, 1990
Design and Airworthiness Requirements for Service Aircraft Volume 2 - Rotorcraft Book 2 (Parts 4 to 6) Part 4: Detail Design and Strength of Materials
GENERAL In the detailed design of the rotoreraft, the variety of materials and parts shall be kept to a minimum consistent with structural efficiency and without unduly sacrificing structure weight....

References

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