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NA 131

DIN Standards Committee Aerospace

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Projects of NA 131

Number: 362

ISO/DIS 14621-1 2025-02-25 Space systems - Electrical, electronic and electromechanical (EEE) parts - Part 1: Parts management More  Comment 
ISO/DTR 20590 2025-02-25 Space systems - Space debris mitigation design and operation manual for launch vehicle orbital stages More  Comment 
ISO/FDIS 21886 2025-02-25 Space systems - Configuration management More  Comment 
DIN EN 3646-011 rev 2025-02-19 Aerospace series - Connectors, electrical, circular, bayonet coupling, operating temperature 175 °C or 200 °C continuous - Part 011: Dummy receptacle - Product standard More  Comment 
DIN EN 3833 2025-02-19 Aerospace series - Bolt, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), passivated - Classification: 1 550 MPa (at ambient temperature)/650 °C - Technical specification; German and English version prEN 3833:2025 More  Comment 
DIN EN 3613 2025-02-18 Aerospace series - Bolt, normal hexagonal head, relieved shank, long thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated - Classification: 1 275 MPa/650 °C; German version FprEN 3613:2026 More  Comment 
DIN EN 3293 2025-02-17 Aerospace series - Bolt, T-head, close tolerance, medium thread length, in heat resisting nickel base alloy NI-P100HT (Inconel® 718), uncoated - Classification: 1 275 MPa/650 °C; German and English version FprEN 3293:2026 More  Comment 
DIN EN 3327 2025-02-17 Aerospace series - Bolts, double hexagon head, close tolerance, medium thread length, in heat resisting nickel base alloy NI-P100HT (Inconel 718), uncoated - Classification: 1 275 MPa/650 °C; German version FprEN 3327:2026 More  Comment 
DIN EN 4131 2025-02-17 Aerospace series - Bolt, normal hexagonal head, coarse tolerance normal shank, medium length thread, in heat resisting nickel base alloy, aluminium IVD coated - Classification: 1 250 MPa (at ambient temperature)/425 °C; German version FprEN 4131:2026 More  Comment 
ISO/TR 25775 2025-02-11 Space systems - Justification of requirements for a spacecraft large constellation More  Comment 

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