SBIR/STTR Research Award

High Pressure Sintered Nanotubes - Fullerenes for Propulsion Systems

Award identifier d0ae3e959f05a406a411c7ec993988f308d5e6ea99eae2c7e275bb21b9947013Awarding agency National Aeronautics and Space Administration

Award amount

$70,000

Program and phase

SBIR · Phase I

Award year

2001

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
DIAMOND MATERIALS INC
Proposal award date
Not reported
Contract end date
Not reported
UEI
CNGFRH5K94P6
Solicitation number
Not reported
Topic code
Not reported

Research abstract

We propose to develop and demonstrate new ablation/erosion resistant carbon material for application in nanosatellite propulsion systems. Our newly invented conductive superhard, high bond strength ¿polymerized¿ fullerene materials will achieve the high ablation and erosion resistance. The new materials called Fullertubite and DiamoniteTM (patent pending) have properties that make them ideal for use in the micro-engines to be used in orbit upkeeping and transfer. The new materials will allow fabrication of nozzles and engine system elements that are subjected to very high temperature gases expanding from the reaction chamber. DiamoniteTM is the third hardest material after diamond and c-BN; it is isotropic, and highly fracture and abrasion resistant. The bonds of the material are predominantly sp3, endowing it with a low sputter rate along with high erosion resistance. It¿s also electrically conductive, which makes it suitable for electrical micropropulsion systems. Fullertubite/DiamoniteTM are formed by the high-pressure (>1 GPa), high-temperature (>400¿C) sintering of nanotubes and C60 fullerenes into an isotropic non-crystalline material using DMIs developed sintering technology. Phase I will focus on proof-of-principle development of Fullertubite/DiamoniteTM materials and determining their ablation/erosion, thermal, mechanical, and electrical properties at engine conditions. In Phase II the Fullertubite/DiamoniteTM micro engine parts will be fabricated and tested in a nanosatellite propulsion systems.

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.

Research funding history

34 SBIR/STTR records share this UEI (1988–2018). Reported award amounts total $7,967,215. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Energy, National Science Foundation

Agency intelligence

National Aeronautics and Space Administration

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