Published By National Aeronautics and Space Administration
Issued about 9 years ago
Summary
Description
This SBIR Phase 1 project shall investigate concept radiator fins that incorporate novel carbon materials for improved performance of segmented high temperature space radiator systems based on heat pipes with attached radiator fins. The novel carbon materials apply to improvements in several critical features: thermal emissivity, in-plane conductivity, fin stiffness, fin/pipe thermal interface, and lightweight shielding against micrometeorites. Phase 1 will obtain system requirements from a prime contractor for nuclear space power, and assess the potential benefits compared with current baseline materials. A small carbon radiator fin component will be fabricated and integrated with a relevant pipe to demonstrate the materials concepts.