共找到 2056 條與 航空與航天用非金屬材料 相關的標準,共 138 頁
Ground simulation method for space radiation effect of non-metallic materials in space environment
Specification for thermally conductive silicone grease for use in spacecraft
本文件規(guī)定了采用惰性氣體熔融-熱導檢測法測定連續(xù)氮化物陶瓷纖維中氮含量的試樣制備、試樣測試、測試結果計算等內(nèi)容。 本文件適用于采用惰性氣體熔融-熱導檢測法測定連續(xù)氮化硅陶瓷纖維、連續(xù)氮化硼陶瓷纖維、連續(xù)硅硼氮陶瓷纖維、連續(xù)硅硼碳氮陶瓷纖維的總氮含量。非連續(xù)氮化物陶瓷纖維及基體的氮含量測試參照本文件。其他陶瓷纖維的氮含量測試參考本文件。
Test methods of continuous nitride ceramic fibers—Part 1:Nitrogen content
本文件規(guī)定了采用惰性氣體熔融-紅外吸收法測定連續(xù)碳化硅纖維中氧含量的試樣制備、.試樣測試、測試結果計算等內(nèi)容。 本文件適用于采用惰性氣體熔融-紅外吸收法測定連續(xù)碳化硅纖維的總氧含量。非連續(xù)碳化硅纖維及基體的氧含量測試參照本文件。其他陶次纖維的氧含量測試參考本文件。
Test methods of continuous silicon carbide fibers—Part 8:Oxygen content
本文件規(guī)定了航天器用導熱硅脂的技術要求、檢驗方法、檢驗規(guī)則、包裝和標志、運輸和貯存。 本文件適用于航天器用導熱硅脂(以下簡稱導熱硅脂)的檢驗、交收和使用。
Specification for silicone grease thermal filler of spacecraft
本文件規(guī)定了采用高頻感應燃燒-紅外吸收法測定連續(xù)碳化硅纖維中碳含量的試樣制備、試樣測試、測試結果計算等內(nèi)容。 本文件適用于采用高頻感應燃燒-紅外吸收法測定連續(xù)碳化硅纖維的總碳含量。非連續(xù)碳化硅纖維及基體的碳含量測試參照本文件。其他陶瓷纖維的碳含量測試參考本文件。
Test methods of continuous silicon carbide fibers—Part 9:Carbon content
Test methods for continuous silicon carbide fiber-Part 6:Resistivity
Test methods for continuous silicon carbide fiber—Part 7 :High temperature strength retention rate
Test methods for continuous silicon carbide fiber—Part 3:Linear density and density
Evaluating method for spacecraft nonmetal materials outgassing in vacuum
Test methods for continuous silicon carbide fiber—Part 1:Size content of filament yarn
Test methods for continuous silicon carbide fiber—Part 4:Tensile properties of filament yarn
Test methods for continuous silicon carbide fiber—Part 2:Diameter of single-filament fiber
Test methods for continuous silicon carbide fiber—Part 5:Tensile properties of single-filament fiber
Evaluating method for spacecraft nonmetal materials outgassing in vacuum
This document specifies the requirements for a two-components flexible polyurethane topcoat to be applied over EN 4687 and/or EN 4688 primers mainly for exterior aerospace applications. The primer and the finish tested to this document will be from the same manufacturer applied i
Aerospace series - Paints and varnishes - Two-components room temperature curing polyurethane finish - High flexibility and chemical agent resistance for military application; German and English version EN 4689:2021
Aerospace series - Paints and varnishes - Two-components room temperature curing polyurethane finish - High flexibility and chemical agent resistance for military application
This European Standard specifies the requirements for a two component polyurethane, topcoat, with a medium degree of resistance to erosion by the effects of rain, available in a range of colours and levels of gloss, to be applied over a primer for aerospace applications on areas where rain erosion at subsonic speeds may be a problem, e.g. leading edges and air intakes. The properties specified in this European Standard are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837 Procedure A and EN 23270 and painted with primer to EN 2435-001 and -002. The ability of the material to be used for a specific application (e.g. alternative substrate, alternative primer, specific drying conditions, etc.) should be determined by supplementary tests to confirm that the requirements of this European Standard are met.
Aerospace series. Paints and varnishes. Cold curing intermediate coat
This document defines tests on the susceptibility to corrosion in a damp atmosphere of metals in contact with vulcanized rubbers.
Aerospace series - Vulcanized rubbers - Test on the susceptibility to corrosion in a damp atmosphere of metals in contact with vulcanized rubbers; German and English version EN 2899:2018
Aerospace series. Non-metallic materials. Foaming structural adhesives. Test methods. Compressive tube shear
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