AEROSPACE REPORT NUMBER: TOR-2005(8583)-2, ELECTRICAL POWER SYSTEMS, DIRECT CURRENT, SPACE VEHICLE DESIGN REQUIREMENTS (11 MAY 2005)

AEROSPACE REPORT NUMBER: TOR-2005(8583)-2, ELECTRICAL POWER SYSTEMS, DIRECT CURRENT, SPACE VEHICLE DESIGN REQUIREMENTS (11 MAY 2005). This standard establishes requirements for direct current (DC) electrical power systems (EPS) for space vehicles. This standard ensures compatibility between the space vehicle DC EPS and all its interfaces, including the utilization equipment. It also ensures that the space vehicle will not be damaged or degraded by certain unintended or anomalous conditions, as described herein.