The Prevention of Electronical Breakdown and Electrostatic Voltage Problems in the Space Shuttle and Its Payloads. Part 2:Design Guides and Operations Considerations.

摘要

The specific electrical discharge problems that can directly affect the shuttle vehicle and its payloads are addressed. General design guidelines are provided to assist flight hardware managers in minimizing these kinds of problems. Specific data are included on workmanship practices and system testing while in low pressure environments. Certain electrical discharge problems that may be unique to the design of the shuttle vehicle itself and to its various mission operational models are discussed.