Multi-Layered Integrated Airframe System

Award Information
Agency:
National Aeronautics and Space Administration
Amount:
$99,927.00
Program:
SBIR
Contract:
NNX10CC54P
Solitcitation Year:
2009
Solicitation Number:
N/A
Branch:
N/A
Award Year:
2010
Phase:
Phase I
Agency Tracking Number:
095173
Solicitation Topic Code:
X9.02
Small Business Information
Fiber Materials, Inc.
5 Morin Street, Biddeford, ME, 04005-4497
Hubzone Owned:
N
Woman Owned:
N
Socially and Economically Disadvantaged:
N
Duns:
048268890
Principal Investigator
 Benjamin Dwyer
 Principal Investigator
 (207) 282-5911
 bdwyer@fibermaterialsinc.com
Business Contact
 David Audie
Title: Business Official
Phone: (207) 282-5911
Email: govt@fibermaterialsinc.com
Research Institution
N/A
Abstract
NASA has a need to develop higher performance ablative thermal protection systems (TPS) than is currently available for future exploration of our solar system's inner and outer planets. Potential missions for these new and/or improved TPS materials include Mars Entry, Descent & Landing, and Mars Sample Return, but the general desire is that these new technologies be capable of cross-cutting mission applications. In addition to improved TPS performance, NASA also has a need for TPS integrated with the sub-structure that will improve thermal efficiency, insulation performance, system thermal-structural performance, and system integrity with the goal of achieving increased system reliability, reduced areal mass, and/or decreased costs over the current state-of-the-art (SOTA). This program will address NASA's need to: 1) Develop higher performing TPS materials to meet the demands of severe mission trajectories such as Mars Sample Return; and 2) Integrate TPS materials with the sub-structure to improve overall robustness and decrease mass. This program's goal is to extend Phenolic Impregnated Carbon Ablator (PICA, TRL=9) and Integrated Composite Structure (ICS, TRL=5) TPS materials to a broader range of flight heat fluxes and performance to address future missions and heatshield designs. The current TRL for the multi-layered TPS system is 3, with an envisioned TRL of 6 at the completion of a successful Phase II program.

* information listed above is at the time of submission.

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