SBIR/STTR Research Award

Flexible Transfer of Regolith in Micro-Gravity and Vacuum

Award identifier 79b602ec5ba247108b3eb33f7377bd21c795ade52ae5abceeed2a16f0e574e77Awarding agency National Aeronautics and Space Administration

Award amount

$124,870

Program and phase

SBIR · Phase I

Award year

2012

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
GRAINFLOW DYNAMICS, INC.
Proposal award date
2012-02-23
Contract end date
2012-08-23
UEI
SKAKGHZYFEM1
Solicitation number
Not reported
Topic code
X1.01

Research abstract

A novel, robust method of collection and transfer of NEO/Phobos material under micro-gravity conditions under vacuum/space environment with minimal loss of volatiles will be developed and its feasibility demonstrated. The same designs can also be utilized in lunar or Martian applications with only minor modifications. Design of the light-weight flexible conveyor ducts will utilize recently verified regolith simulation software to assure that the concepts are viable under microgravity conditions, and prototypes will be tested under vacuum conditions in Phase-1 (and under micro-gravity during Phase-2). Depending on the drill-head/feeder design selected, these flexible transfer ducts could be used in extraction of material from depths of a meter or more below the surface. Under Martian conditions a 1-cm-diameter conveying duct could deliver 5 kg/hr of material to a processing station for extraction/processing of volatiles. Trade-off studies during Phase-1 will determine potential power saving (if any) in larger diameter conveying ducts (e.g., 1.5 or 2cm dia) and/or the power requirements in a smaller diameter conveying duct (e.g. 0.5 cm dia) under Martian conditions. Unlike conventional screw conveyors, these flexible transfer ducts would be robust to oversize material up to a size of one-half the transfer duct radius. Coupled with an oversize-rejection inlet feeder, the system could provide high reliability transfer of loose regolith with one or two major moving parts. Modular designs are possible, as is the incorporation of energy-efficient ultrasonic (or percussion) drill heads, or sensors near a sub-surface inlet.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

12 SBIR/STTR records share this UEI (2008–2019). Reported award amounts total $1,787,406. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: National Aeronautics and Space Administration, Department of Defense

Agency intelligence

National Aeronautics and Space Administration

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