PROTECTING AEROSPACE ASSETS FROM
SPACE ENVIRONMENTAL EFFECTS

HII specializes in the preparation and application of coatings for spacecraft and satellites. 

Six Decades of Experience

As a leading provider of commercial spacecraft thermal control products​, HII’s AMCL has a 60-year history in advanced thermal space coatings science and chemistry, an outstanding reputation for solving complex problems quickly and a heritage of success for material and services.

Our engineers pioneered the development of unique materials for the protection of aerospace structures and components from space environmental effects. HII has produced materials for NASA, including the Gemini and Apollo missions; the International Space Station (ISS); and the U.S. Department of Defense.

Streamlined Finishing Process

We developed a “super finishing” process followed by the application of military specified anti-corrosion coatings that increase the life of a metal part by 20%. We also employ Air Force Research Laboratory- and NASA-approved materials for use based on rigorous space simulation exposure. AMCL is Quality Management System ISO 9001:2015 certified.

Alignment with NASA Specifications

AMCL has worked with NASA since shortly after that agency’s creation in 1958, designing and applying mission-critical thermal coatings that protect satellites and spacecraft from the harsh conditions of outer space. We have been on the cutting edge of interplanetary missions and manned missions to the International Space Station (ISS).

Our coatings conform to NASA’s strict specifications, taking into account custom data about orbital patterns, environmental factors like temperature and radiation level, and more. The coatings help control the external temperature of spacecraft and limit UV radiation absorption, which allows instruments to operate more effectively.

State-of-the-Art Production Facilities

With a complete inventory of optical testing, mixing and application equipment in state-of-the-art facilities, we can tailor thermal control coatings to fill our customers’ specific needs.

Learn more about our large-scale production facilities, on-site test equipment and performance specifications.

  • Six Decades of Experience
  • Streamlined Finishing Process
  • Alignment with NASA Specifications
  • State-of-the-Art Production Facilities

Six Decades of Experience

As a leading provider of commercial spacecraft thermal control products​, HII’s AMCL has a 60-year history in advanced thermal space coatings science and chemistry, an outstanding reputation for solving complex problems quickly and a heritage of success for material and services.

Our engineers pioneered the development of unique materials for the protection of aerospace structures and components from space environmental effects. HII has produced materials for NASA, including the Gemini and Apollo missions; the International Space Station (ISS); and the U.S. Department of Defense.

Streamlined Finishing Process

We developed a “super finishing” process followed by the application of military specified anti-corrosion coatings that increase the life of a metal part by 20%. We also employ Air Force Research Laboratory- and NASA-approved materials for use based on rigorous space simulation exposure. AMCL is Quality Management System ISO 9001:2015 certified.

Alignment with NASA Specifications

AMCL has worked with NASA since shortly after that agency’s creation in 1958, designing and applying mission-critical thermal coatings that protect satellites and spacecraft from the harsh conditions of outer space. We have been on the cutting edge of interplanetary missions and manned missions to the International Space Station (ISS).

Our coatings conform to NASA’s strict specifications, taking into account custom data about orbital patterns, environmental factors like temperature and radiation level, and more. The coatings help control the external temperature of spacecraft and limit UV radiation absorption, which allows instruments to operate more effectively.

State-of-the-Art Production Facilities

With a complete inventory of optical testing, mixing and application equipment in state-of-the-art facilities, we can tailor thermal control coatings to fill our customers’ specific needs.

Learn more about our large-scale production facilities, on-site test equipment and performance specifications.

Performance of Aerospace Coatings

STANDARD (NON-ELECTROSTATIC DISSIPATIVE) THERMAL CONTROL MATERIAL SYSTEMS (TCMS)

CoatingComposition / Temperature CapabilityTypical Optical Properties
(α ± 0.02 | EN ± 0.05)
Applications
Z-93PWhite Inorganic 800°C0.15 | 0.90Highest stability and temperature capability, well-suited for long-term missions (used on ISS)
S13GP:6N/LO-1White Organic Flexible 200°C0.15 | 0.90High stability, silicone base improves durability and ease of application, ideal for most LEO missions
S13NT:6N/LO-1Off-White Organic Flexible 200°C0.29 | 0.89Variation of S13GP:6N/LO-1 for intermediate absorptance needs
MH21:6N/LOBlack Organic Flexible 200°C0.98 | 0.90High absorptance coating, silicone base, made with HII’s “black glass” pigment
MH2200Flat Black Optical Absorber 530°C0.96 | 0.90Best suited for absorbing surfaces to prevent light reflection

ELECTROSTATIC DISSIPATIVE THERMAL CONTROL MATERIAL SYSTEMS (TCMS)

CoatingComposition / Temperature CapabilityTypical Optical Properties
(α ± 0.02 | EN ± 0.05)
Typical Surface Resistivity
(Ω/▯)
Applications
Z93C55White Inorganic 500°C0.15 | 0.9010⁶ to 10⁸Conductive analog to Z-93P, ideal for longer missions outside of LEO (used on Mars Rovers/Reconnaissance, JUNO)
DS13N:6N/LO-HPWhite organic flexible 200°C0.15 | 0.90107 to 10¹⁰Conductive analog to S13GP:6N/LO-1, ideal for electrostatically sensitive surfaces
MH21:6NC/LOBlack organic flexible 200°C0.98 | 0.9010⁶ to 10⁸Conductive analog to MH21:6N/LO for high absorptance/ESD needs

Notes:
α = solar absorbance
EN = total normal emittance
Ω/▯ = ohms per square
Application by gas spraying: all Curing at room temperature: all Good thermal shock resistance: all Atomic oxygen (AO) resistant: all
Outgassing: inorganic, total mass loss (TML) = 0.10 to 0.25 and collectable volatile condensible material (CVCM) = 0.00 to 0.01

For questions or pricing, contact [email protected]

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