Standard No.:	QJ 2301-1992
English Name:	Specification for Altitude Simulation Test of Solid Rocket Motor
Chinese Name:	固体火箭发动机高空模拟试验规范
Chinese Classification:	V70    Spacecraft in general
Professional Classification:	QJ    Professional Standard - Aerospace
Issued on:	1992-02-26
Implemented on:	1992-11-1
Status:	valid
Language:	English
File Format:	PDF
Word Count:	5000 words
Price(USD):	150.0
Delivery:	via email in 1 business day

Specification for high-altitude simulation test of solid rocket motors 1 Subject content and application scope This standard specifies the equipment composition and requirements, test procedures and data processing methods for the high-altitude simulation tests of solid rocket motors (hereinafter referred to as the "motors"). This standard is applicable to the passive-ejection high-altitude simulation test of large and medium solid rocket motors, and may also be referred to for the high-altitude simulation test of small motors. 2 Normative references QJ 28 Calculation method for static accuracy of pressure sensors QJ 1004 Firing test procedures of solid rocket motors QJ 1045 Specification for measuring thrust of solid rocket motors QJ 1046 Specification for measuring pressure of solid rocket motors QJ 1047 Specification for processing pressure-time and thrust-time data of solid rocket motors QJ 1118 Specification for design of test frame of solid rocket motors QJ 1188 Terminology for solid rocket motors QJ 1370 Specification for measuring ignition pressure of solid rocket motors QJ 1590 Specification for measuring vacuum pressure of test environment for solid rocket motors QJ 1625 Parameter symbols of solid rocket motors QJ 1647 Specification for measuring surface temperature of rocket motor QJ 1658 Methods of air tight test for solid rocket motor QJ 1816 Displacement measurement methods for solid rocket motors QJ 1817 Vibration measurement methods for solid rocket motors QJ 1818 Strain measurement methods for solid rocket motors QJ 2037 Safety technical requirements for ground hot firing test of solid rocket motors 3 Terms 3.1 vacuum cabin a cabin-type device that forms and maintains the high-altitude and low-pressure environment required for high-altitude simulation test and enables the motor to work in it

1 Subject content and application scope 2 Normative references 3 Terms 4 Test equipment 5 Test procedures and methods 6 Data processing and test report