Deployable reflector in the form of a reuleaux triangle for a space observation instrument
Résumé
The invention relates to a deployable reflector (RP) for a space observation instrument, comprising a selected number of deployable reflective elements (E1a-E3b) which, once deployed in a first position, together define a reflective surface in the form of a Reuleaux triangle (RD) with a closed convex curve having a width that is constant as a function of the direction.