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Position: Chinese Standard in English/QJ 2328-1992
QJ 2328-1992   Test method for temperature accelerated aging of composite solid propellant (English Version)
Standard No.: QJ 2328-1992 Status:superseded remind me the status change

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Word Count: 8500 words Translation Price(USD):350.0 remind me the price change

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Implemented on:1992-12-30 Delivery: via email in 1 business day

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,2006-5-1,1992-12-30,8B8B21DAAA2741761422613085307
Standard No.: QJ 2328-1992
English Name: Test method for temperature accelerated aging of composite solid propellant
Chinese Name: 复合固体推进剂储存老化试验方法
Professional Classification: QJ    Professional Standard - Aerospace
Issued on: 1992-03-24
Implemented on: 1992-12-30
Status: superseded
Superseded by:QJ 2328A-2005 Test method for temperature accelerated aging of composite solid propellant
Superseded on:2006-5-1
Target Language: English
File Format: PDF
Word Count: 8500 words
Translation Price(USD): 350.0
Delivery: via email in 1 business day
QJ 2328-1992 Composite solid propellant storage aging test method 1 Subject content and application scope This standard specifies the test equipment, test conditions, test steps, test methods, aging test mathematical model and calculation method for high-temperature accelerated aging test of composite solid propellant (hereinafter referred to as propellant) by oven aging method. This standard is applicable to accelerated aging test and service life prediction of propellant carton. 2 Normative references GB 4883 Statistical interpretation of data - Detection and treatment of outliers in the normal sample QJ 912 Method for determination of burning rate of composite solid propellant strips by underwater acoustic emission QJ 915 Method for determination of burning rate, burning rate pressure index and burning rate temperature sensitivity coefficient of composite solid propellant strips (target line method) QJ 924 Unidirectional tensile test method for composite solid propellants QJ 1113 Test specimens for performance testing of composite solid propellants 3 Aging performance evaluation 3.1 This standard specifies that unidirectional tensile properties and burning rate of the strips are used as performance evaluation parameters. If other properties are to be added as aging performance evaluation parameters, it can be decided by the engine design unit and the propellant development unit through consultation. 3.2 The limit value of aging performance evaluation parameters is the limit index to meet the requirements of engine design and use, which shall be put forward by the engine design unit and the propellant development unit through consultation. 3.3 The limit value can be expressed either as an absolute value of the test data or as a percentage (relative value) of the change in the original value. 4 Test equipment and instruments 4.1 Electric heating oil bath thermostat (hereinafter referred to as oven)
1 Subject content and application scope 2 Normative references 3 Aging performance evaluation 4 Test equipment and instruments 5 Specimen preparation 6 Test conditions 7 Test procedures 8 Data processing and test report Annex A Data processing method (Supplement) Annex B Correlation coefficient γ value and t distribution (unilateral) (Supplement) Annex C Calculation examples (Reference) Additional explanation
Referred in QJ 2328-1992:
*GB 4883-1985 Statistical interpretation of data; Detection and handling of outlying observations in normal sample
*QJ912-
*QJ915-
*QJ 924-1985 Uniaxial Tensile Test Methods for Composite Solid Propellant
*QJ 1113-1987 Sample for Composite Solid Propellant Performance Test
QJ 2328-1992 is referred in:
*QJ 2215A-2005 The items and methods for performance characterization of composite solid propellant
Code of China
Standard
QJ 2328-1992   Test method for temperature accelerated aging of composite solid propellant (English Version)
Standard No.QJ 2328-1992
Statussuperseded
LanguageEnglish
File FormatPDF
Word Count8500 words
Price(USD)350.0
Implemented on1992-12-30
Deliveryvia email in 1 business day
Detail of QJ 2328-1992
Standard No.
QJ 2328-1992
English Name
Test method for temperature accelerated aging of composite solid propellant
Chinese Name
复合固体推进剂储存老化试验方法
Chinese Classification
Professional Classification
QJ
ICS Classification
Issued by
Issued on
1992-03-24
Implemented on
1992-12-30
Status
superseded
Superseded by
QJ 2328A-2005 Test method for temperature accelerated aging of composite solid propellant
Superseded on
2006-5-1
Abolished on
Superseding
Language
English
File Format
PDF
Word Count
8500 words
Price(USD)
350.0
Keywords
QJ 2328-1992, QJ/T 2328-1992, QJT 2328-1992, QJ2328-1992, QJ 2328, QJ2328, QJ/T2328-1992, QJ/T 2328, QJ/T2328, QJT2328-1992, QJT 2328, QJT2328
Introduction of QJ 2328-1992
QJ 2328-1992 Composite solid propellant storage aging test method 1 Subject content and application scope This standard specifies the test equipment, test conditions, test steps, test methods, aging test mathematical model and calculation method for high-temperature accelerated aging test of composite solid propellant (hereinafter referred to as propellant) by oven aging method. This standard is applicable to accelerated aging test and service life prediction of propellant carton. 2 Normative references GB 4883 Statistical interpretation of data - Detection and treatment of outliers in the normal sample QJ 912 Method for determination of burning rate of composite solid propellant strips by underwater acoustic emission QJ 915 Method for determination of burning rate, burning rate pressure index and burning rate temperature sensitivity coefficient of composite solid propellant strips (target line method) QJ 924 Unidirectional tensile test method for composite solid propellants QJ 1113 Test specimens for performance testing of composite solid propellants 3 Aging performance evaluation 3.1 This standard specifies that unidirectional tensile properties and burning rate of the strips are used as performance evaluation parameters. If other properties are to be added as aging performance evaluation parameters, it can be decided by the engine design unit and the propellant development unit through consultation. 3.2 The limit value of aging performance evaluation parameters is the limit index to meet the requirements of engine design and use, which shall be put forward by the engine design unit and the propellant development unit through consultation. 3.3 The limit value can be expressed either as an absolute value of the test data or as a percentage (relative value) of the change in the original value. 4 Test equipment and instruments 4.1 Electric heating oil bath thermostat (hereinafter referred to as oven)
Contents of QJ 2328-1992
1 Subject content and application scope 2 Normative references 3 Aging performance evaluation 4 Test equipment and instruments 5 Specimen preparation 6 Test conditions 7 Test procedures 8 Data processing and test report Annex A Data processing method (Supplement) Annex B Correlation coefficient γ value and t distribution (unilateral) (Supplement) Annex C Calculation examples (Reference) Additional explanation
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Keywords:
QJ 2328-1992, QJ/T 2328-1992, QJT 2328-1992, QJ2328-1992, QJ 2328, QJ2328, QJ/T2328-1992, QJ/T 2328, QJ/T2328, QJT2328-1992, QJT 2328, QJT2328