Structure design criterion for turbojet and turbofan engine of missile
1 Scope
This standard specifies the design basis, design criteria, design contents, design procedures, design methods and design verification test items for the structure design of turbojet and turbofan engine of missile.
This standard is applicable to the structure design of turbojet and turbofan engine of missile (hereinafter referred to as "engine").
2 Normative references
The following normative documents contain provisions which, through reference in this standard, constitute provisions of this standard. For dated references, subsequent amendments (excluding corrections) to, or revisions, of any of these publications do not apply to this standard. However, parties to agreements based on this standard are encouraged to investigate the possibility of applying the most recent editions of the normative documents indicated below. For undated references, the latest edition applies.
GJB 151A-1997 Electromagnetic emission and susceptibility requirements for military equipment and subsystems
GJB 368A-1994 General maintainability program for material
GJB 450-1988 General reliability program for materiel development and production
GJB 813-1990 Reliability modeling and prediction
GJB 900-1990 General program for system safety
GJB 1371-1992 Logistic support analysis for materiel
GJB 1391-1992 Procedure for failure mode, effects and criticality analysis
GJB 3057-1997 General specification for lubricating system of turbine engine for aircraft
GJB 3811-1999 The compatibility requirements of ignition system characteristic and burner design for gas turbine engine
GJB 3816-1999 General technical requirements for aeroengine line system
HB/Z 134-1988 Design guide for geared fuel pump in engine fuel control system
3 Design basis
The engine structure design assignment proposed for the engine as a whole.
