We propose to break the two-mission space exploration cycle (remote survey eventually followed by in situ sensing) by creating mission architectures that perform both remote survey and in situ sampling. Through enabling technologies, such as high-accuracy quantum, or cold-atom, inertial sensors based on light-pulse atom interferometry (LPAI), and the extreme miniaturization of space components into fully functional spacecraft-on-a-chip systems (ChipSats), these combined missions can perform decadal-class science with greatly reduced time scales and risk.
More »Adoption of dual exploration architectures may short circuit the long, slow cycle of missions to inaccessible bodies by eliminating the need for separate precursor and follow-up missions. Additionally, the dual architecture possesses inherent flexibility that enables the design of adaptive, event-driven missions that are very different from traditional, largely pre-planned missions. A survey of historical and current missions finds that opportunities for exploration are becoming less frequent, causing the flexibility and dual-nature elements of each mission to become more common. The dual exploration architecture takes these trends to their far conclusion, attempting to eliminate precursor and follow-up missions while still returning more scientific payoff. A study of the future of planetary science goals through the decadal survey reveals broad applicability of dual missions to solve mysteries that cannot be answered with a traditional mission architecture. These missions fall into three broad classes: choosing a local target from a global survey, dynamic/reactive science, and global in-situ networks.
More »Organizations Performing Work | Role | Type | Location |
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The Charles Stark Draper Laboratory, Inc. | Lead Organization | Non-Profit Institution | Cambridge, Massachusetts |
Cornell University | Supporting Organization | Academia | Ithaca, New York |