Code of China Chinese Standard Classification Professional Classification ICS Classification Latest
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Standard No. Title Price(USD) Delivery Status Add to Cart
HB/Z 286.3-1996 Guide for Design and Implementation of Monitoring System for Aviation Gas Turbine Engine - Grease Monitoring $360.00 via email in 1~5 business day valid
HB/Z 286.4-1996 Guide for Design and Implementation of Monitoring System for Aviation Gas Turbine Engine - Vibration Monitoring $225.00 via email in 1~3 business day valid
HB/Z 286.5-1996 Guide for Design and Implementation of Monitoring System for Aviation Gas Turbine Engine - Service Life Monitoring $255.00 via email in 1~3 business day valid
HB/Z 286.6-1996 Guide for Design and Implementation of Monitoring System for Aviation Gas Turbine Engine - Temperature Monitoring $435.00 via email in 1~5 business day valid
HB/Z 312-1998 Guideline on the Installation and Design of Aircrafts Gas Turbine Auxiliary Power Device $1050.00 via email in 1~5 business day valid
HB/Z 313-1998 Design and Installation Requirements for Airentrainment System of Aircraft Engine $195.00 via email in 1~3 business day valid
HB/Z 320-1998 Determination of Helicopter Turbine Engine Entraining $120.00 via email in 1~3 business day valid
QJ 1047-1992 Data Processing Specifications for Pressure - Time and Thrust - Time of Solid Rocket Engine $660.00 via email in 1~5 business day valid
QJ 1813.2-2005 Determining methods for viscosity and pot life of composite solid propellant slurry Part 2:Method by rotational viscometer $120.00 immediately valid
QJ 3192-2004 General specification for turbojet engines of missile $210.00 immediately valid
QJ 3193-2004 Structure design criterion for turbojet and turbofan engine of missile $210.00 immediately valid
QJ 3231-2005 Reliability evaluation for solid rocket motors $270.00 via email in 1~3 business day valid
QJ 3236-2005 Measuring method for negative thrust of static firing test of solid rocket motor $150.00 immediately valid
QJ 3237-2005 Measurement method for geometrical thrust deviation and off-set of solid rocket motor $150.00 immediately valid
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