Space systems. Spacecraft-to-launch-vehicle interface control document1 Scope The purpose of this International Standard is to provide spacecraft (SC) and launch vehicle (LV) organizations with the general format for presenting the interface control document (ICD) that verifies and controls the compatibility between SC and LV for a dedicated mission. This International Standard addresses the definition of the mission, the compatibility of the SC with the LV environment, including all mechanical, electrical, radio

BS EN 1047-2 beneficial in improving the safety of occupants

Vehicle regulatory authorities

The basic width is the nominal widthb as defined in 2

C# application developers

The guidelines in BS EN 61076-4-113 provide you with the standardized detail specification for two-part connectors that enable you to provide a superior quality product to your customers

BS EN 10212 specifies a spectrophotometric method for the determination of arsenic in steel and iron

Soap and detergent manufacturers

Lifting tables

insulation

Home care ventilators for ventilator-dependent patients

The specifications cover structures travelling vertically between two predefined levels along a guided path where the inclination to the vertical does not exceed 15° and supported or sustained by wire ropes

People responsible for business travel