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THERMAL PROTECTION

Orion Heat Shield System

ACTIVE
Heat ShieldTYPE
Lockheed MartinMANUFACTURER
970MASS (KG)
0 (passive ablative)POWER (W)
N/A (single shield, margin in ablator depth)REDUNDANCY
ABOUT ORION HEAT SHIELD SYSTEM

When NASA’s Orion capsule comes home from the Moon, it slams into Earth’s atmosphere at about 25,000 miles per hour and faces temperatures near half that of the Sun’s surface. The heat shield is the one piece of hardware standing between that fire and the astronauts inside.

Quick facts

  • What it protects: the base of Orion, NASA’s crew capsule for the Artemis missions to the Moon.
  • Diameter: 16.5 feet (5 meters) — the largest heat shield of its type ever built.
  • Reentry speed from the Moon: about 25,000 mph, roughly Mach 32 (nearly 35 times the speed of sound).
  • Peak surface temperature: around 5,000 degrees Fahrenheit (about 2,760 degrees Celsius), roughly half the temperature of the Sun’s surface.
  • Crew-side temperature: stays in the mid-70s Fahrenheit.
  • Material: Avcoat, an updated version of the ablator flown on the Apollo capsules.
  • Build: about 186 machined Avcoat blocks, each roughly 1 to 3 inches thick, bonded to a carbon-fiber skin.

What it is and how it works

The Orion heat shield is an ablative thermal protection system — “ablative” meaning it is designed to char and slowly burn away in a controlled way, carrying heat off the spacecraft rather than letting it soak into the structure. It does not reflect the heat or merely insulate against it. It sacrifices itself.

As Orion plunges into the atmosphere, friction with the air superheats the shield’s outer surface. The Avcoat material — an epoxy-novolac resin held in a fiberglass honeycomb matrix — reacts by pyrolyzing, meaning the resin breaks down chemically and gives off gases. The charred outer layer slowly erodes away, carrying enormous amounts of heat with it. Think of it like the way sweat cools your skin: energy leaves with the material that departs, keeping what is underneath cool. During the uncrewed Artemis I flight, the cabin interior stayed in the mid-70s Fahrenheit while the outside raged near 5,000.

One detail matters greatly: the char layer must be permeable — full of tiny paths — so the gases forming beneath it can vent out instead of building up pressure. The broad, blunt shape of the shield helps too, pushing the hottest layer of shocked air away from the vehicle. Orion can fly a “skip” entry, dipping into the upper atmosphere and skipping back out using aerodynamic lift before its final descent, or a steeper direct entry.

Why it matters

This is the single most safety-critical system for crew survival on a lunar return. Coming back from the Moon is far hotter and faster than returning from low Earth orbit, and the roughly 13-minute reentry offers no second chance. The shield took about 15 years and over 1,000 tests to develop. Building it from about 186 pre-molded blocks, rather than hand-filling Apollo’s 300,000 honeycomb cells, cut application time by roughly 75 percent.

That block design also produced a famous engineering lesson. On Artemis I in 2022, the Avcoat shed its charred layer unevenly, leaving cavities. NASA’s investigation found the cause in the gentle, drawn-out heating of the skip-entry path: the mild heating slowed char formation while gases kept building underneath, and where the char was not permeable enough, trapped gas pressure cracked the Avcoat and popped pieces off. Ground arc-jet tests had used higher heating rates, so the char vented normally and the effect went unseen.

Notable flights

  • Apollo (1960s-70s): the heritage program whose Avcoat ablator and blunt-body reentry approach Orion’s shield is directly descended from.
  • EFT-1 (2014): an early Orion flight test that used an Avcoat shield in the older honeycomb style.
  • Artemis I (2022): first lunar-return flight of the shield, uncrewed; survived reentry but revealed the uneven char loss that triggered a two-year investigation.
  • Artemis II (splashdown April 2026): first crewed lunar flyby. Rather than redesign the shield, NASA changed operations — a steeper, shorter entry — and made future Avcoat more uniformly permeable. Char loss dropped sharply, the capsule landed within about 2.9 miles of its target, and NASA declared the system performed as expected.
SPECIFICATIONS
CategoryThermal Protection
SubcategoryHeat Shield
ManufacturerLockheed Martin
Mass970 kg
Power0 W
Dimensions5.0 m diameter, ~38 mm ablator depth
RedundancyN/A (single shield, margin in ablator depth)
StandardHuman-rated lunar return
StatusActive
First UseDecember 5, 2014
OPERATING PRINCIPLE
AVCOAT ablative material in fiberglass honeycomb structure absorbs and re-radiates reentry heating; charring and outgassing create boundary layer that blocks convective heat
KEY SPECIFICATIONS
materialAVCOAT
diameter_m5.0
max_temp_c2760
entry_velocity_km_s11
MASS CONVERSIONS
Kilograms970.0 kg
Pounds2,138.5 lbs
VEHICLES USING ORION HEAT SHIELD SYSTEM (2)
  • Orion MPCV
  • Artemis missions

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