← ALL HEAT SHIELDS
LOCKHEED MARTIN

AFRSI (Advanced Flexible Reusable Surface Insulation)

Flexible BlanketRETIRED (SHUTTLE)Reusable
816
°C
MAX TEMPERATURE
1,500°F
0.04
W/m·K
THERMAL CONDUCTIVITY
0.14
KG/M³
DENSITY
19-25 mm
THICKNESS
TYPICAL
2.2 kg/m²
KG/M²
MASS PER AREA
1
VEHICLES
PROTECTED
THERMAL RATING
816°C / 3,000°C

AFRSI (Advanced Flexible Reusable Surface Insulation) is a flexible blanket thermal protection system by Lockheed Martin. Rated to 816°C. Status: Retired (Shuttle).

When the Space Shuttle came home from orbit, it slammed into the atmosphere fast enough to glow. AFRSI is the quilted blanket that kept the cooler parts of the spacecraft from cooking on the way down.

Quick facts

  • Full name: Advanced Flexible Reusable Surface Insulation (sometimes called a Flexible Insulation Blanket, or FIB).
  • What it is: A lightweight, sewn silica-fiber blanket used as a thermal protection system (TPS) — the heat shielding that keeps a spacecraft’s structure from overheating during reentry.
  • Temperature limit: Works where reentry temperatures stay below about 1,200 F (about 650 C).
  • Weight: About 8 to 9 pounds per cubic foot (roughly 130 to 145 kg/m3) — very light.
  • Made of: 99.8% pure silica fiber batting, sandwiched between a tough outer woven-silica fabric and an inner glass fabric, quilted together with silica thread.
  • Built by: Developed at NASA’s Ames Research Center; installed on the orbiters by Rockwell International.
  • Coverage: Discovery and Atlantis each carried roughly 1,900 square feet of it.

What it is and how it works

AFRSI is essentially a high-tech quilt. Its thick inner layer is a batting of pure silica fibers — silica is the same glassy material as sand and ordinary glass. That batting is a superb insulator because the tiny fibers and the air trapped between them carry heat very poorly. During reentry, the hot outer surface radiates heat energy back out to the air, while the blanket keeps the aluminum airframe (the metal frame of the vehicle) underneath it cool.

The blanket has three jobs split across three layers. The tough outer woven-silica fabric faces the rushing airflow and tolerates high heat. The thick silica batting in the middle does the insulating. The inner glass fabric, made of borosilicate (a heat-resistant glass), bonds the blanket to the spacecraft’s skin.

Because it is a flexible blanket rather than a stiff tile, it could be cut into large pieces, draped over curved surfaces, and glued directly onto the structure. Think of the difference between tiling a wall with thousands of small ceramic squares versus rolling out one big sheet of wallpaper — the blanket approach is far faster and cheaper. It is reusable across many flights, and small damage could be fixed simply by re-sewing frayed threads or patching it.

Why it matters

AFRSI replaced thousands of heavier, more fragile rigid white ceramic tiles, known as LRSI, on the cooler upper surfaces of later orbiters. Those tiles were slow and expensive to make, install, and inspect one by one. Swapping most of them for blankets cut weight, slashed the time and cost of preparing the vehicle between flights, and demanded far less maintenance — all while delivering roughly the same thermal protection. It proved that large, curved areas of a returning spacecraft could be shielded with a sewn fabric rather than countless individual tiles, a lesson that shaped later flexible-insulation systems.

Where it fits and its limits

AFRSI evolved from an earlier blanket called FRSI, which used Nomex felt and could only handle about 370 C. Switching to silica fiber raised the usable temperature to around 650 C. In the Shuttle’s lineup of shields, AFRSI sits in the middle: FRSI for the coolest zones, AFRSI for warm-but-not-searing areas, rigid silica tiles (LRSI and HRSI) for hotter zones, and reinforced carbon-carbon for the white-hot nose and wing leading edges. AFRSI only works on the orbiter’s relatively cool leeward (upper) surfaces — the searing windward belly and nose still needed rigid black tiles and carbon-carbon.

Notable examples

  • Challenger flew AFRSI first, on its Orbital Maneuvering System (OMS) pods — the bulges housing the engines used to maneuver in orbit. After the STS-6 flight, inspectors found about ten damaged blankets and lost cover fabric on roughly twenty more.
  • The C-9 coating was NASA’s response to that damage: a ceramic surface coating that toughened the outer fabric and could patch minor wear.
  • Discovery and Atlantis each used about 1,900 square feet of AFRSI to replace the majority of their rigid white LRSI tiles.
  • Conformal Reusable Insulation (CRI), a later flexible-blanket system studied for reusable launch vehicles, built directly on the AFRSI approach. The underlying silica-blanket technology also became a NASA Spinoff used in high-temperature industrial insulation.
🛡Material TypeFlexible Blanket
🌡Max Temperature816°C (1,500°F)
Thermal Conductivity0.04 W/m·K
🔥AblativeNo
ReusableYes
Density0.14 kg/m³
📏Thickness19-25 mm
Mass per Area2.2 kg/m² kg/m²

Nextel 440 outer fabric, Q-fiber felt batting, S-Glass inner fabric

Space Shuttle (upper surfaces, payload bay doors)
🚀First MissionSTS-6 (Challenger)
📅First FlightApril 4, 1983
🏭ManufacturerLockheed Martin
🟢StatusRetired (Shuttle)

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