Simulated space debris impact experiments on toughened laminated thin solar cell cover glass

Abstract

Increasing demands on the design criteria of space craft components have driven efforts to develop advanced space debris ground simulation techniques suitable to be incorporated into a space environmental effects chamber. A laser driven flyer method suitable in such a chamber was used to conduct an initial investigation of space debris impact on a new toughened solar cell coverglass material. Damage characteristics, including mechanical damage and contamination generated by impact with a 3mm diameter, 3 micron thick aluminum particle accelerated to 4.5 km/s, were looked at. Scanning electron microscopy, optical microscopy, and spectrophotometry were used to measure the mechanical damage and the loss of solar transmission. Because of the limited number of impact tests made in this initial study a quantitative analysis was not possible. However, much insight was obtained from the observed damage.