The Suess-Urey (S-U) mission has been proposed as a NASA Discovery mis
sion to return samples of matter from the Sun to the Earth for isotopi
c and chemical analyses in terrestrial laboratories to provide a major
improvement in our knowledge of the average chemical and isotopic com
position of the solar system. The S-U spacecraft and sample return cap
sule will be placed in a halo orbit around the L1 Sun-Earth libration
point for two years to collect solar wind ions which implant into larg
e passive collectors made of ultra-pure materials. Constant Spacecraft
-Sun-Earth geometries enable simple spin stabilized attitude control,
simple passive thermal control, and a fixed medium gain antenna. Low d
ata requirements and the safety of a Sun-pointed spinner, result in ex
tremely low mission operations costs. Copyright (C) 1997 Elsevier Scie
nce Ltd.