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Position: Chinese Standard in English/QJ 2038.2-1991
QJ 2038.2-1991   Test method for interface bonding strength of solid rocket motor chamber- Shear method (English Version)
Standard No.: QJ 2038.2-1991 Status:valid remind me the status change

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Target Language:English File Format:PDF
Word Count: 3500 words Translation Price(USD):120.0 remind me the price change

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Implemented on:1991-9-1 Delivery: via email in 1 business day

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,,1991-9-1,2AA7BE7C39EA3B701419317432142
Standard No.: QJ 2038.2-1991
English Name: Test method for interface bonding strength of solid rocket motor chamber- Shear method
Chinese Name: 固体火箭发动机燃烧室界面粘接强度测试方法 剪切法
Chinese Classification: V72    Spacecraft power system
Professional Classification: QJ    Professional Standard - Aerospace
Issued on: 1991-01-24
Implemented on: 1991-9-1
Status: valid
Target Language: English
File Format: PDF
Word Count: 3500 words
Translation Price(USD): 120.0
Delivery: via email in 1 business day
QJ 2038.2-1991 Test method for interface bonding strength of solid rocket motor chamber- Shear method 1 Subject content and application scope This standard specifies the specimen preparation, test procedure, and test result processing of testing the combination shear bonding strength of the chamber case, insulation, liner, and propellant of solid rocket motor (hereinafter referred to as motor). This standard is applicable to testing the combination shear bonding strength of the motor chamber case, insulation, liner, and propellant, as well as the testing the shear bonding strength of the motor chamber case with fiber winding, and metal parts are used instead of fiber winding parts during specimen production. 2 Normative references QJ 2038.1 Test method for interface bonding strength of solid rocket motor chamber - Unstick test 3 Test principle The insulation, liner, and propellant with the same area are bonded between two parallel metal plates, and the tensile force is applied in the direction parallel to the bonding surface to measure the stress when the specimen reaches shear failure. 4 Equipment
1 Subject content and application scope 2 Normative references 3 Test principle 4 Equipment 5 Specimen 6 Test procedure 7 Testing result processing
Referred in QJ 2038.2-1991:
*QJ 2038.1-1991
QJ 2038.2-1991 is referred in:
*QJ 1488A-2004 General specification for chamber insulation liner and stress release boot of solid rocket motor
Code of China
Standard
QJ 2038.2-1991  Test method for interface bonding strength of solid rocket motor chamber- Shear method (English Version)
Standard No.QJ 2038.2-1991
Statusvalid
LanguageEnglish
File FormatPDF
Word Count3500 words
Price(USD)120.0
Implemented on1991-9-1
Deliveryvia email in 1 business day
Detail of QJ 2038.2-1991
Standard No.
QJ 2038.2-1991
English Name
Test method for interface bonding strength of solid rocket motor chamber- Shear method
Chinese Name
固体火箭发动机燃烧室界面粘接强度测试方法 剪切法
Chinese Classification
V72
Professional Classification
QJ
ICS Classification
Issued by
Issued on
1991-01-24
Implemented on
1991-9-1
Status
valid
Superseded by
Superseded on
Abolished on
Superseding
Language
English
File Format
PDF
Word Count
3500 words
Price(USD)
120.0
Keywords
QJ 2038.2-1991, QJ/T 2038.2-1991, QJT 2038.2-1991, QJ2038.2-1991, QJ 2038.2, QJ2038.2, QJ/T2038.2-1991, QJ/T 2038.2, QJ/T2038.2, QJT2038.2-1991, QJT 2038.2, QJT2038.2
Introduction of QJ 2038.2-1991
QJ 2038.2-1991 Test method for interface bonding strength of solid rocket motor chamber- Shear method 1 Subject content and application scope This standard specifies the specimen preparation, test procedure, and test result processing of testing the combination shear bonding strength of the chamber case, insulation, liner, and propellant of solid rocket motor (hereinafter referred to as motor). This standard is applicable to testing the combination shear bonding strength of the motor chamber case, insulation, liner, and propellant, as well as the testing the shear bonding strength of the motor chamber case with fiber winding, and metal parts are used instead of fiber winding parts during specimen production. 2 Normative references QJ 2038.1 Test method for interface bonding strength of solid rocket motor chamber - Unstick test 3 Test principle The insulation, liner, and propellant with the same area are bonded between two parallel metal plates, and the tensile force is applied in the direction parallel to the bonding surface to measure the stress when the specimen reaches shear failure. 4 Equipment
Contents of QJ 2038.2-1991
1 Subject content and application scope 2 Normative references 3 Test principle 4 Equipment 5 Specimen 6 Test procedure 7 Testing result processing
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Keywords:
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