SASSI: Subsystems for Automated Subsurface Sampling Instruments

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX09CA90C
Agency Tracking Number: 074934
Amount: $599,842.00
Phase: Phase II
Program: SBIR
Awards Year: 2009
Solicitation Year: 2007
Solicitation Topic Code: S5.03
Solicitation Number: N/A
Small Business Information
460 W 34th Street, New York, NY, 10001-2320
DUNS: 131364820
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Kris Zacny
 Principal Investigator
 (510) 207-4555
Business Contact
 Chris Chapman
Title: President
Phone: (646) 459-7802
Research Institution
Autonomous surface sampling systems are necessary, near term, to construct a historical view of planetary significant events; as well as allow for the identification of materials useful for ISRU activities. Paramount to this is exploration missions capable of in-situ analysis of core samples that deliver the stratigraphy of the target. These sample handling technologies must be developed to meet a broad range of potential requirements, including a variety of rock or subsurface materials, rigorous sample preservation requirements, and the general problem of autonomous operation in the presence of dust and with limited resources. Honeybee seeks to develop critical subsystems for a small, low-mass, low-power Rotary-Percussive Corer (RoPeC) capable of autonomous sample acquisition and delivery from a depth of 5 cm. Specific attention will be given to the tall-pole items including the core break-off, retention, delivery, rotary-percussive drive, and gas flushing subsystems. Near term applications include the Astrobiology Field Laboratory and Mars Sample Return missions. Previous coring tool development has focused on integration and far-horizon proof of concepts; resulting in complete systems designed around specific requirements. The path forward lies in maturing specific aspects of designs quickly. The Phase 1 research has resulted in a survey of existing sampling systems as well as a conceptual design of the RoPeC with a focus on modularity. In Phase 2, Honeybee will mature the design of RoPeC subsystems; including the integration of a percussive voice coil actuator developed by the Jet Propulsion Laboratory for the Mars Science Laboratory (MSL) Powder Acquisition Drill System. A focus on modularity will ensure that subsystems can be redesigned independently; enabling the acquisition of core samples in targets including MEPAG suggested rocks, MSL Mars analogs and Phoenix analogs. This will lead to the a TRL of 5-6.

* Information listed above is at the time of submission. *

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