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TEXTRON SYSTEMS

AVCOAT

AblativeACTIVEAblative
2,800
°C
MAX TEMPERATURE
5,072°F
0.08
W/m·K
THERMAL CONDUCTIVITY
0.51
KG/M³
DENSITY
40 mm
THICKNESS
TYPICAL
20.4 kg/m²
KG/M²
MASS PER AREA
2
VEHICLES
PROTECTED
THERMAL RATING
2,800°C / 3,000°C

AVCOAT is a ablative thermal protection system by Textron Systems. Rated to 2,800°C. Status: Active.

AVCOAT is an epoxy novolac resin ablative heat shield material originally developed by Avco Corporation for the Apollo program. It was applied in a honeycomb matrix and protected astronauts during lunar return reentries at speeds up to 11 km/s. AVCOAT has been revived and modernized for NASA’s Orion Multi-Purpose Crew Vehicle.

🛡Material TypeAblative
🌡Max Temperature2,800°C (5,072°F)
Thermal Conductivity0.08 W/m·K
🔥AblativeYes
ReusableNo
Density0.51 kg/m³
📏Thickness40 mm
Mass per Area20.4 kg/m² kg/m²

Epoxy novolac resin with silica and phenolic microballoons in fiberglass honeycomb

Apollo Command Module
Orion MPCV
🚀First MissionApollo 4
📅First FlightNovember 9, 1967
🏭ManufacturerTextron Systems
🟢StatusActive

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