Detail of QJ 2438A-2005

Introduction of QJ 2438A-2005

Technological requirements for packaging spacecraft 1 Scope This standard specifies the packing principle, technological support for packing, technological requirements for packing, technological procedures for packing, test methods and inspection rules of packing containers and packing segments of spacecraft (including cabin). This standard is applicable to packing and the design, manufacture, test and acceptance of and packing boxes of various spacecrafts. 2 Normative references The following documents contain provisions which, through reference in this standard, constitute provisions of this standard. For dated references, subsequent amendments (excluding corrections) to, or revisions of, any of these publications do not apply. However parties to agreements based on this standard are encouraged to investigate the possibility of applying the most recent edition of the normative documents indicated below. For undated references, the latest edition of the normative document applies. GB 146.1 Rolling stock gauge for standard gauge railways GB/T 191 Packaging - Pictorial marking for handling of goods GB 1589 Outside dimension limits of motor vehicles GB/T 4122.1 Packaging terms - Part 1: Basic GB/T 4122.2 Packaging terms - Part 2: Machinery GB/T 4122.3 Packaging terms - Part 3: Protection GB/T 4857.9 Packaging - Basic tests for transport packages - Part 9: Water spray test GJB 2203A-2005 Cleanliness and contamination control requirements for satellite product QJ 1558-1988 Test method for materials outgassing performance in vacuum QJ 2249-1992 General technical requirements for satellite hoisting, overturning, parking and transportation QJ 2574A-1998 Safety requirements for satellite assembly QJ 2850-1996 Prevention and control for foreign object debris (FOD) space products   3 Terms and definitions For the purposes of this standard, the terms and definitions given in GB/T 4122.1, GB/T 4122.2 and GB/T 4122.3 and the following apply. 3.1 packing container containers used for loading spacecraft and meeting the requirements of storage and transportation, which are also called packing boxes 3.2 packing segment assembly containing spacecraft after packing 4 Packing principles 4.1 The packing shall be firm, safe, simple and easy to disassemble and assemble. 4.2 The packing generally adopts integral packing method. If necessary, the packing may be carried out in different cabins. In principle, only one product with its accessories, spare parts and accompanying documents shall be packed in one packing box, and non-matching products shall not be included. Products and spare parts/accessories (such as antenna, solar wing, storage battery, camera and multilayer thermal insulation material of thermal control system) which belong to the same spacecraft may be packed separately.

Contents of QJ 2438A-2005

Foreword I 1 Scope 2 Normative references 3 Terms and definitions 4 Packing principles 5 Technological support for packing 6 Technological requirements for packing 7 Flow chart of packing technology 8 Inspection items and test methods of the packing box 9 Maintenance, storage and caring of the packing boxes Annex A (Normative) Inspection items and test methods of spacecraft packing boxes