| CPC G02B 23/06 (2013.01) [G02B 7/022 (2013.01); G02B 7/183 (2013.01)] | 6 Claims |

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1. A versatile space telescope adapted for interfacing with a spacecraft and an instrument module, comprising:
a. an aluminum barrel shaped body having a longitudinal optical axis and a proximal end adapted for positioning adjacent the spacecraft via a plurality of threaded holes for capturing a support structure secured to the spacecraft and a distal end adapted for positioning adjacent the instrument module;
b. a first diamond turned, aspheric aluminum mirror having an entrance pupil and positioned adjacent the distal end of the barrel shaped body and sharing the longitudinal optical axis;
c. a second diamond turned, aspheric aluminum mirror creating an exit pupil and positioned adjacent the proximal end of the barrel shaped body and sharing the longitudinal optical axis;
d. at least one heater integrated with the barrel shaped body to provide thermal control;
e. a hex plate attached to the barrel shaped body, positioned in longitudinally spaced relation from the first mirror and sharing the longitudinal optical axis;
f. a plano-convex aspheric lens supported by the hex plate and positioned along the longitudinal optical axis; and
g. a plurality of flexures interconnecting the hex plate to the first mirror.
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