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Results for “ablative materials”

Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.

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All sourcesNASA NTRSDOE OSTI
NASA NTRS2006

Carbon Nanotube-enhanced Carbon-phenolic Ablator Material

Phenolic impregnated carbon ablator (PICA) is a thermal protection system (TPS) material developed at NASA Ames Research Center in the mid-90 s for Discovery missions. It was used on the Stardust return capsule heat shield which successfully executed the highest speed Earth entry to date on January 15, 2006. PICA is a porous fibrous carbon insulation infiltrated with phenolic resin, and is an excellent ablator that is effective for heating rates up to 1000 W/sq cm. It is one of several candidate TPS materials for the next generation of crewed spacecraft for Lunar and Mars missions. We will describe an ongoing research effort at NASA to improve mechanical properties of the phenolic matrix with carbon nanotubes. The aim is two-fold: to increase overall TPS strength during reentry and to improve Micrometeoroid/Orbital Debris (MMOD) protection in space. The former requires at least a good dispersion of nanotubes in phenolic, while the latter also requires covalent bonding between them to couple and transfer impact energy effectively from matrix to nanotubes. We will discuss the required chemical functionalization of nanotubes, processing issues and test results.

Nikolaev, P.↗
NASA NTRS1993

An evaluation of ablative materials for a lunar transfer vehicle aerobrake

An evaluation of the utility of an ablative thermal protection system (TPS) for use on a lunar mission return aerobrake has been completed. Requirements are established and criteria developed specifically for the ablator application. A quantitative and qualitative multi-attribute utility analysis is employed to establish a relative ranking among candidates and a performance threshold. A review of the applicable existing ablator material database is made and appropriate thermochemical/melting ablation analysis is employed to evaluate thermal performance. Ablatives are shown to be potentially both performance capable and cost effective in single-use roles. Reusable surface insulation is also shown to be competitive as an ablator with certain modifications.

Lane, J. G.↗