GJB 6345-2008
The flight test reguirements of design qualification for turboshaft engine of military helicopter (English Version)
- Standard No.
- GJB 6345-2008
- Language
- Chinese, Available in English version
- Release Date
- 2008
- Published By
- Military Standard of the People's Republic of China-General Armament Department
- Latest
- GJB 6345-2008
- Scope
- This standard stipulates the general requirements for design and finalization flight tests of helicopter turboshaft engines and the detailed requirements for test conditions, test contents and methods, and measurement parameters of each test item. This standard applies to turboshaft engine design finalization flight test.
GJB 6345-2008 Referenced Document
- GJB 1017-1990 Specifications for ground and flight testing of aviation gas turbine propulsion systems
- GJB 2103A-1997 Aviation gas turbine power plant terminology and symbols
- GJB 242-1987 General specification for aerospace turboprop and turboshaft engines
- GJB 243-1987 Aviation gas turbine power plant flight test specifications
- GJB 3457-1998 Military helicopter design final flight test outline and reporting requirements
- HB 0-89-1990 Commonly used technical volume symbols for aviation turbine engines
- HB 0-90-1990 Aviation turbine engine performance section symbols and term designators
GJB 6345-2008 history
- 2008 GJB 6345-2008 The flight test reguirements of design qualification for turboshaft engine of military helicopter
