Aerospace series. Nuts, anchor, self-locking, floating, two lug, reduced series, with counterbore, in steel, cadmium plated, MoS2 lubricated. Classification: 1 110 MPa (at ambient temperature)/235 °C
€165.00
Programme Management. Definition justification and qualification. A guide to drawing up the definition justification plan and of the definition justification dossier
€316.00
Space product assurance. Electrical, electronic and electromechanical (EEE) components
€404.00
Aerospace series. Connectors, electrical, rectangular, modular. Operating temperature 175 °C continuous Specification of performance and contact arrangements
€269.00
Space product assurance. Commercial electrical, electronic and electromechanical (EEE) components
BS EN 4165-025. Aerospace series. Connectors, electrical, rectangular, modular. Operating temperature 175 °C continuous. Part 025. Single module receptacle. Product standard
€23.00
Space product assurance. Processing and quality assurance requirements for hard brazing of metallic materials for flight hardware
BS EN 3841-101. Aerospace series. Circuit breakers. Test methods Part 101. Management of the retention qualification
BS EN 4165-025. Aerospace series. Connectors, electrical, rectangular, modular. Operating temperature 175 °C continuous Part 025. Single module receptacle. Product standard
BS EN 4165-015. Aerospace series. Connectors, electrical, rectangular, modular. Operating temperature 175 °C continuous Part 015. Round chimney for accessory (1 per module cavity), 2 and 4 modules. Product standard
Space systems. Safety and compatibility of materials Determination reactivity system/component with aerospace propellants
€193.00
Aerospace series. Rotorcraft immersion suits. Requirements, testing and marking
€374.00
Aerospace series. Rotorcraft constant wear lifejackets. Requirements, testing and marking
Vertiports. Infrastructure and equipment for vertical take-off and landing (VTOL) of electrically powered cargo unmanned aircraft systems (UAS)
Space projects. Programme management. Dependability assurance requirements
