In Earth orbit, atomic oxygen (AO) erodes and degrades many spacecraft mate
rials. Several sensors have been employed to make in situ measurements of t
hese oxygen atom fluxes, yet none has proved suitable for general applicati
on to microsatellites. We have investigated the potential of thin-film zinc
oxide (ZnO) AO sensors. It is known that single crystal and thin-film semi
conductor sensors may be used to measure fluxes of low-energy (thermal) oxy
gen atoms. This work extends the principle to the measurement of hypertherm
al (high energy) oxygen atoms ina ground-based simulation facility. It is f
ound that, upon exposure to AO, the conductance of the ZnO sensors decrease
s. Moreover, the rate of sensor conductance change is proportional to the f
lux of oxygen atoms. Two sensors, which were manufactured simultaneously, d
emonstrated very similar responses when exposed concurrently to hypertherma
l AO. Further experiments showed that the sensors were not affected by flux
es of molecular oxygen, but were influenced by ultraviolet (UV) radiation.
A ZnO film covered with silica - to prevent the action of AO - was used to
examine the influence of UV, which was shown to cause a small, permanent ch
ange of the conductance of the semiconductor (C) 2000 Elsevier Science S.A.
All rights reserved.