Microspacecraft

Under a study contract, the Italian Space Agency (ASI) developed the mechanical system concept for a Mars Microspacecraft to launch in a twin configuration on an Ariane V ASAP (Auxiliary Payload). As a member a multi-disciplined team, ASI developed the mechanical configuration and preliminary structure design for the spacecraft in two configurations, a probe carrier and an orbiter.

References

Anderson, Nikka. "Micro-spacecraft, Instrumentation, & Electronics". NASA. http://library.gsfc.nasa.gov/SubjectGuides/Micro.htm. Retrieved 2007-08-30. 

Mauritz, A.; Patel, B.. "Science-Enabling MicroSpacecraft Constellations for Mars". Concepts and Approaches for Mars Exploration. STI (NASA). pp. 215. http://adsabs.harvard.edu/abs/2000came.work..215M. Retrieved 2007-08-30.