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Position: Chinese Standard in English/QJ 2258A-2001
QJ 2258A-2001   Measure Methods for Mass Characteristic of Spacecraft (English Version)
Standard No.: QJ 2258A-2001 Status:valid remind me the status change

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,,2002-2-1,95B9E5891A1E950E1412780291970
Standard No.: QJ 2258A-2001
English Name: Measure Methods for Mass Characteristic of Spacecraft
Chinese Name: 航天器质量特性测试方法
Chinese Classification: V70    Spacecraft in general
Professional Classification: QJ    Professional Standard - Aerospace
Issued on: 2001-11-15
Implemented on: 2002-2-1
Status: valid
Superseding:QJ 2258-1992
Target Language: English
File Format: PDF
Word Count: 4000 words
Translation Price(USD): 120.0
Delivery: via email in 1 business day
Measure methods for mass characteristic of spacecraft 1 Scope This standard specifies the test methods for the mass, centroid, moment of inertia and inertia product of satellites and spacecraft. This standard is applicable to the mass characteristic measurement of satellites, spacecraft and their cabin sections and components (hereinafter referred to as "specimen"). 2 Normative references The following documents contain provisions which, through reference in this text, constitute provisions of this standard. For dated references, subsequent amendments to, or revisions of, any of these publications (exclude errata) do not apply. However, parties of agreements based on this part of the directives are encouraged to investigate the possibility of applying the most recent editions of the normative documents indicated below. For undated references, the latest edition of the normative document referred to applies. GJB 3756-1999 Expression and evaluation of uncertainty in measurement QJ 2574A-1998 Safety requirements for satellite assembly 3 General 3.1 Environmental requirements In addition to the environmental requirements of the specimen, the test environment shall also meet the following requirements: a) The daily temperature fluctuation during the test shall not be greater than 2°C; b) There shall be no vibration, noise, airflow and electromagnetic interference that affect the test accuracy. 3.2 Test technical documents Relevant technical documents shall be prepared before the test and meet the following requirements: a) The technical status, structural dimensions, test items, uncertainty and test coordinate system of the specimens specified in the design documents; b) The process documents shall be based on the test scheme, test equipment, test procedure and measurement accuracy specified in the design documents; c) The design documents and process documents shall pass the technical review of relevant departments. 3.3 Test equipment and tooling
Foreword i 1 Scope 2 Normative references 3 General 4 Detailed requirements Annex A (Normative) Evaluation of uncertainty of test results
Referred in QJ 2258A-2001:
*GJB3756-1999
*QJ 2574A-1998 Safety Requirements for Satellite General Installation
Code of China
Standard
QJ 2258A-2001  Measure Methods for Mass Characteristic of Spacecraft (English Version)
Standard No.QJ 2258A-2001
Statusvalid
LanguageEnglish
File FormatPDF
Word Count4000 words
Price(USD)120.0
Implemented on2002-2-1
Deliveryvia email in 1 business day
Detail of QJ 2258A-2001
Standard No.
QJ 2258A-2001
English Name
Measure Methods for Mass Characteristic of Spacecraft
Chinese Name
航天器质量特性测试方法
Chinese Classification
V70
Professional Classification
QJ
ICS Classification
Issued by
Issued on
2001-11-15
Implemented on
2002-2-1
Status
valid
Superseded by
Superseded on
Abolished on
Superseding
QJ 2258-1992
Language
English
File Format
PDF
Word Count
4000 words
Price(USD)
120.0
Keywords
QJ 2258A-2001, QJ/T 2258A-2001, QJT 2258A-2001, QJ2258A-2001, QJ 2258A, QJ2258A, QJ/T2258A-2001, QJ/T 2258A, QJ/T2258A, QJT2258A-2001, QJT 2258A, QJT2258A
Introduction of QJ 2258A-2001
Measure methods for mass characteristic of spacecraft 1 Scope This standard specifies the test methods for the mass, centroid, moment of inertia and inertia product of satellites and spacecraft. This standard is applicable to the mass characteristic measurement of satellites, spacecraft and their cabin sections and components (hereinafter referred to as "specimen"). 2 Normative references The following documents contain provisions which, through reference in this text, constitute provisions of this standard. For dated references, subsequent amendments to, or revisions of, any of these publications (exclude errata) do not apply. However, parties of agreements based on this part of the directives are encouraged to investigate the possibility of applying the most recent editions of the normative documents indicated below. For undated references, the latest edition of the normative document referred to applies. GJB 3756-1999 Expression and evaluation of uncertainty in measurement QJ 2574A-1998 Safety requirements for satellite assembly 3 General 3.1 Environmental requirements In addition to the environmental requirements of the specimen, the test environment shall also meet the following requirements: a) The daily temperature fluctuation during the test shall not be greater than 2°C; b) There shall be no vibration, noise, airflow and electromagnetic interference that affect the test accuracy. 3.2 Test technical documents Relevant technical documents shall be prepared before the test and meet the following requirements: a) The technical status, structural dimensions, test items, uncertainty and test coordinate system of the specimens specified in the design documents; b) The process documents shall be based on the test scheme, test equipment, test procedure and measurement accuracy specified in the design documents; c) The design documents and process documents shall pass the technical review of relevant departments. 3.3 Test equipment and tooling
Contents of QJ 2258A-2001
Foreword i 1 Scope 2 Normative references 3 General 4 Detailed requirements Annex A (Normative) Evaluation of uncertainty of test results
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Keywords:
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