Subsurface Coring Sampler System

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$599,049.00
Award Year:
2002
Program:
SBIR
Phase:
Phase II
Contract:
NAS3-02091
Award Id:
56914
Agency Tracking Number:
001882
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
204 Elizabeth St., New York, NY, 10012
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
n/a
Principal Investigator:
Shaheed Rafeek
Engineering Group Leader
(212) 966-0661
rafeek@hbrobotics.com
Business Contact:
Chris Chapman
President
(212) 966-0661
chapman@hbrobotics.com
Research Institute:
n/a
Abstract
Honeybee Robotics is proposing a new type of planetary and small bodies sample acquisition and sample handling system that can operate in extreme environments and satisfy crucial mission related science and sample return requirements. Many in-situ instruments are currently only capable of handling small amount of samples (0.1 - 1.0 cc) while missions with sample return requirements have a need for large volume of samples (100-500 cc). The proposed Subsurface Coring Sampler System (SCSS) is capable of acquiring small samples for in-situ science and larger samples for sample return by adjusting the sample volume. Another unique feature of the SCSS is its ability to obtain stratigraphy maintained surface and subsurface cores of varying lengths. Once the cores are obtained, the SCSS can function as precision material handling system, transferring the cores to sample return containers or depositing smaller sections of the cores to in-situ instruments for analysis. This low mass, low power sampling system will be developed with multiple mission applicability in mind, interfacing with a majority of existing in-situ instruments being developed by other NASA centers such as GSFC (CHARGE) and Ames (CIDEX). The SCSS will also be developed with interface commonality to a multi-chamber sample return container currently being developed by Honeybee Robotics for the Jet Propulsion Laboratory.

* information listed above is at the time of submission.

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