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Fullerene-Based Ablative Coolant for Small, Chemical, Space Propulsion Systems

Award Information

Agency:
National Aeronautics and Space Administration
Branch:
N/A
Award ID:
22840
Program Year/Program:
1994 / SBIR
Agency Tracking Number:
22840
Solicitation Year:
N/A
Solicitation Topic Code:
N/A
Solicitation Number:
N/A
Small Business Information
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No
 
Phase 1
Fiscal Year: 1994
Title: Fullerene-Based Ablative Coolant for Small, Chemical, Space Propulsion Systems
Agency: NASA
Contract: N/A
Award Amount: $70,000.00
 

Abstract:

Fullerenes - the recently discovered closed cage forms of carbo - have unique and unprecedented pure carbon based thermal properties. Advanced materials based on fullerenes and fullerenes all by themselves are lightweight, long lived, environmentally benign and are materials that have very low thermal conductivity and which sublime at high temperatures. These properties make fullerenes and fullerene based advanced materials ideally suited for ablation based applications. This proposal will establish, as part of Phase I work, the proof- of-concept that fullerenes will ablatively cool combustion chambers and nozzles. The effort envisioned is to first deposit fullerene films of varying thickness onto an experimental sized combustion chamber and nozzle. Next, the surface will be exposed to high temperature flame environment and the temperature of the combustion chamber wall will be monitored. The Phase II work will focus on optimizing the performance of fullerene films as ablative coolants.

Principal Investigator:

Tapesh Yadav
6025741980

Business Contact:

Small Business Information at Submission:

Materials & Electrochemical
7960 South Kolb Road Tucson, AZ 85706

EIN/Tax ID:
DUNS: N/A
Number of Employees: N/A
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No