The construction and optical performance of Fabry-Perot etalons for:spacefl
ight are considered. Optical mounts with sufficient mechanical firmness to
handle intense vibration loads cause significant distortion of etalon plate
s, degrading the etalon resolving power and peak transmittance. A mount is
described that combines mechanical robustness with very low plate distortio
n. An etalon mounted in this manner survived spaceflight-level vibration te
sting, in two axes, without damage or degradation. The defect finesse of th
is etalon, measured after the vibration tests, was 46, at a wavelength of 5
32 nm, about three times the values achieved with previous Fabry-Perot etal
ons for spaceflight. (C) 2000 Society of Photo-Optical instrumentation Engi
neers. [S0091-3286(00)03201-3].