SBIR/STTR
Graded Density Carbon Bonded Carbon Fiber (CBCF) Preforms for Lightweight Ablative Thermal Protection Systems (TPS), Phase I
Project Introduction
FMI currently manufactures Phenolic Impregnated Carbon Ablator (PICA) material for Thermal Protection Systems (TPS) systems, such as the Stardust Sample Return Capsule and the Mars Science Laboratory Aeroshell. FMI plans to further develop TPS in support of future sample return missions such as MoonRise and OSIRIS-REx. Development of a PICA TPS with reduced mass, thermal performance enhancements, and optimized single-section near net-shape preforms are enabling technologies for these applications. It is the objective of the proposed program to develop a graded density preform to achieve a reduction in PICA TPS areal mass, to assess the performance of such a TPS, and to develop a plan for manufacturing scale-up.
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Primary U.S. Work Locations and Key Partners
| Organizations Performing Work | Role | Type | Location |
|---|---|---|---|
Ames Research Center
(ARC)
|
Lead Organization | NASA Center | Moffett Field, California |
| Fiber Materials, Inc. | Supporting Organization | Industry | Biddeford, Maine |
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Organizational Responsibility
Responsible Mission Directorate:
- Space Technology Mission Directorate (STMD)
Lead Center / Facility:
- Ames Research Center (ARC)
Responsible Program:
- SBIR/STTR
Project Management
Program Director:
Program Manager:
Project Duration
Start: Feb 2011
End: Sep 2011
Technology Areas
Primary:
- TX14 Thermal Management Systems
- TX14.3 Thermal Protection Components and Systems
- TX14.3.1 Thermal Protection Materials
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