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Guidelines for Strength Design of Military Aircraft

Guidelines for Strength Design of Military Aircraft, Total:14 items.

In the international standard classification, Guidelines for Strength Design of Military Aircraft involves: Aerospace electric equipment and systems, Electromagnetic compatibility (EMC), Corrosion of metals, Aircraft and space vehicles in general.

Professional Standard - Aviation, Guidelines for Strength Design of Military Aircraft

HB/Z 287-1996 Design guidelines for strength and stiffness of aircraft control systems
HB/Z 322-1998 Guidelines for Design of Composite Structures for Military Aircraft
HB/Z 302-1997 Design guide for civil aircraft power supply system
HB/Z 404-2013 Civil Aircraft Electrical Installation Design Guidelines
HB/Z 298-1997 Civil Aircraft Avionics Design Guidelines
HB/Z 185-1990 Lightning Protection and Lap Design Guidelines for Civil Aircraft
HB/Z 402-2013 Design guidelines for integrated modular avionics systems for civil aircraft
HB/Z 401-2013 Environmental design guidelines for packaging and interfacing of integrated modular avionics systems for civil aircraft

Aeronautical Radio Inc., Guidelines for Strength Design of Military Aircraft

ARINC 607-3-1998 Design Guidance for Avionic Equipment 1986; Includes Supplements 1-3

British Standards Institution (BSI), Guidelines for Strength Design of Military Aircraft

BS G 257-2:1998 Design of electromagnetic hazard protection of civil aircraft - Guide to protection
BS G 257-1:1998 Design of electromagnetic hazard protection of civil aircraft - Guide to theory and threats

Professional Standard - Electron, Guidelines for Strength Design of Military Aircraft

SJ 20985-2008 Technological design guidelines for corrosion prevention and control In military electronic installation

Military Standard of the People's Republic of China-General Armament Department, Guidelines for Strength Design of Military Aircraft

GJB/Z 150.4-2011 Safety Design Guide for Military Electronic Equipment Part 4: Protection against Mechanical Hazards

Society of Automotive Engineers (SAE), Guidelines for Strength Design of Military Aircraft

SAE ARP94910-2012 Aerospace - Vehicle Management Systems - Flight Control Design, Installation and Test of, Military Unmanned Aircraft, Specification Guide for