Microspacecraft

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Under a study contract, 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 in 4 weeks the mechanical configuration and preliminary structure design for the spacecraft in two configurations: a probe carrier and an orbiter.

[edit] References

Anderson, Nikka. Micro-spacecraft, Instrumentation, & Electronics. NASA. Retrieved on 2007-08-30.

(07/2000) "Science-Enabling MicroSpacecraft Constellations for Mars". Concepts and Approaches for Mars Exploration: 215, STI (NASA). Retrieved on 2007-08-30.