Aeroglaze Z306 black polyurethane paint Z306

Porous, moisture-curing polyurethane coating with carbon pigment (binder and carbon pigment named in the LDEF S0069 paper)

Also known as AEROGLAZE Z306

Aeroglaze Z306 is a flat black, moisture-curing polyurethane coating sold by Socomore and distributed by Silmid.

8 sources · Updated 2026-11-01 · CC BY 4.0

Evidence level

5 of 5

Flown or field-proven

Absorb solar energy

0.96 solar absorptivity

Radiate heat

0.90 to 0.91 normal emissivity

Stay low in outgassing

1.0 % TML and 0.02 % CVCM

Recipe, share of the weight

  • not printed in any source readPolyurethane binder
  • not printed in any source readCarbon pigment

Best for

Matte black interior surfaces, instrument baffles and stray-light control in spacecraft, with a solar absorptance of 0.96 and a normal emittance of 0.90 to 0.91 as printed in the leaflet and the NASA 2014 paper

Weakest at

Atomic oxygen in low Earth orbit: on the LDEF leading edge the Z306 surface roughened and its solar absorptance rose, and the LDEF S0069 paper says unprotected Z302 and Z306 erode at the binder and carbon pigment

Risk at a glance

  • People Moderate. Sensitizer risk from isocyanates
  • If it fails Moderate. Atomic oxygen erosion of the binder and carbon pigment
  • Corrosion No data. No corrosion data recorded

Why it exists

Aeroglaze Z306 is a flat black polyurethane coating for spacecraft thermal control and stray-light control. The Silmid leaflet prints a solar absorptivity of 0.96, a normal emissivity of 0.90, a total mass loss of 1.0 % and a CVCM of 0.02 %. The 2014 NASA paper prints a solar absorptance of 0.96 and a normal emittance of 0.91 for a 2.0 to 3.0 mil film, and gives Z306 as an example of a polyurethane black coating for stray-light control on interior surfaces such as instrument baffles.

Recipe

Porous, moisture-curing polyurethane coating with carbon pigment (binder and carbon pigment named in the LDEF S0069 paper)

Aeroglaze Z306 is a moisture-curing polyurethane coating with carbon pigment, per the Silmid product page and the LDEF S0069 paper. Polyurethanes are typically made by reacting a diisocyanate with a polyol, per Wikipedia. The Z306 formulation, its isocyanate, its polyol and the pigment share are not printed in any source read.

What Z306 is made of
IngredientShare of the weightWhat it does
Polyurethane binder not printed in any source read Moisture-curing polyurethane binder, the film-forming part of the paint; the LDEF S0069 paper names the binder as the part that erodes under atomic oxygen
Carbon pigment not printed in any source read Black pigment; the LDEF S0069 paper names the carbon pigment as the part that erodes under atomic oxygen

Weight shares are as printed in the sources.

What it can do

Absorb solar energy

0.96 solar absorptivity

measured

The Silmid leaflet prints a solar absorptivity of 0.96 for AEROGLAZE Z306, and the 2014 NASA paper prints a solar absorptance of 0.96 for a 2.0 to 3.0 mil Aeroglaze Z306 film under ASTM E903-82.

Radiate heat

0.90 to 0.91 normal emissivity

measured

The leaflet prints a normal emissivity of 0.90, and the NASA 2014 paper prints a normal emittance of 0.91 under ASTM E408-71. The two values come from different sources and test methods, so both are shown.

Stay low in outgassing

1.0 % TML and 0.02 % CVCM

measured

The leaflet prints a total mass loss of 1.0 % and a CVCM of 0.02 % for AEROGLAZE Z306, both obtained by a modified cure or bake-out schedule.

How it compares

The Silmid leaflet also lists Aeroglaze Z307 and the gloss white Aeroglaze A276 with their own absorptivity, emissivity, TML and CVCM values, and the NASA 2014 paper lists Black MAC coatings with their own absorptance and emittance values. Those values belong to other products and are not recorded in this profile. For Z307 the NASA paper and the leaflet print different normal emissivity figures, so the two sources are kept separate rather than merged. The Z306 values come from different test schedules and thicknesses than some of those rows, so they are not a ranking.

The same measurements for each material, so you can compare them. Each row names the key condition under the value; the full conditions and methods are in the numbered notes under Technical details.

Benchmarks
MeasurementZ306
Thermal behavior and safety
Thermal emittance after LDEF M0003-8 exposure, Chemglaze Z306 (NASA Boeing paper)0.94 -13
Physical and electrical
Coating thickness range, Aeroglaze Z306 black polyurethane (NASA 2014 paper)2 mils7
Other measurements
Solar absorptivity, AEROGLAZE Z306 (manufacturer leaflet)0.96 -1
Normal emissivity, AEROGLAZE Z306 (manufacturer leaflet)0.9 -2
Total mass loss (TML), AEROGLAZE Z3061 %3
Collected volatile condensable material (CVCM), AEROGLAZE Z3060.02 %4
Solar absorptance, Aeroglaze Z306 black polyurethane (NASA 2014 paper)0.96 -5
Normal emittance, Aeroglaze Z306 black polyurethane (NASA 2014 paper)0.91 -6
Change in solar absorptance (delta alpha s), Z306 wake-positioned LDEF specimens-0.04 -8
Solar absorptance before LDEF EOIM III exposure, Chemglaze Z306 flight sample EOIM3-4-1 (NASA 1995 paper)0.955 -9
Solar absorptance after LDEF EOIM III exposure, Chemglaze Z306 flight sample EOIM3-4-1 (NASA 1995 paper)0.96 -10
Initial solar absorptance of the Z306 coating before LDEF M0003-8 exposure (NASA Boeing paper)0.95 -11
Solar absorptance after LDEF M0003-8 exposure, Chemglaze Z306 (NASA Boeing paper)0.93 -12

Why choose it, and why not

Good for

  • Matte black baffles and interior surfaces: solar absorptance 0.96 and normal emittance 0.91 on a 2.0 to 3.0 mil film (NASA 2014 paper).
  • Low-outgassing black coatings: TML of 1.0 % and CVCM of 0.02 % as printed on the Silmid leaflet, under a modified bake-out schedule.

Watch out for

  • Atomic oxygen: on the LDEF leading edge, Z306 roughened and its solar absorptance rose, and unprotected Z302 and Z306 erode at the binder and carbon pigment.
  • Wake exposure: two LDEF wake specimens showed a change in solar absorptance of about -0.04 (S0069 paper, Figure 13).
  • Isocyanates: the product contains diisocyanates, which are restricted in Great Britain according to the Silmid page.
  • No temperature range, cure schedule or Z306 humidity result was read, so the operating limits are not recorded.

Aeroglaze Z306 is a flat black polyurethane coating with a solar absorptance of 0.96 and a normal emittance of 0.90 to 0.91 as printed in two sources, low TML and CVCM values under a modified bake-out, and documented atomic-oxygen erosion on LDEF. Its operating temperature range, cure schedule and any humidity ageing data are not read in this run, so they are not recorded.

Technical details

For scientists and researchers. Everything above comes from the record below: every number with its method, its conditions and its source.

Other names and standards

The same grade under other systems, as datasheets and standards print them. Each code was checked against the page it comes from.

Other names and standards
SystemCodes
Trade nameAEROGLAZE Z306

Notes

The method, full conditions and any caveat for the numbered rows above.

Notes for the numbered rows
#MeasurementMethodConditionsCaveat
1Solar absorptivity, AEROGLAZE Z306 (manufacturer leaflet)Typical value printed on the manufacturer leafletproduct AEROGLAZE Z306, matte black topcoatbasis dimensionless; the leaflet does not print the test method or film thickness—
2Normal emissivity, AEROGLAZE Z306 (manufacturer leaflet)Typical value printed on the manufacturer leafletproduct AEROGLAZE Z306, matte black topcoatbasis dimensionless; the leaflet does not print the test method or film thickness—
3Total mass loss (TML), AEROGLAZE Z306Printed on the manufacturer leaflet; the footnote says the values come from a modified cure and/or bake-out schedule and refers users to the NASA outgassing databaseproduct AEROGLAZE Z306basis obtained by a modified cure and/or bake-out schedule, as the leaflet footnote states—
4Collected volatile condensable material (CVCM), AEROGLAZE Z306Printed on the manufacturer leaflet; the same footnote appliesproduct AEROGLAZE Z306basis obtained by a modified cure and/or bake-out schedule, as the leaflet footnote states—
5Solar absorptance, Aeroglaze Z306 black polyurethane (NASA 2014 paper)Measured with an AZ Technology LPSR-300 spectral reflectometer, as printed on the slideproduct Aeroglaze Z306, black polyurethanethickness 2.0-3.0 mils as printedmethod as printed ASTM E903-82, reflectance from 0.25 to 2.8 microns at a 15 degree angle of incidence—
6Normal emittance, Aeroglaze Z306 black polyurethane (NASA 2014 paper)Measured with a Gier-Dunkle DB-100 infrared reflectometer, as printed on the slideproduct Aeroglaze Z306, black polyurethanethickness 2.0-3.0 mils as printedmethod as printed ASTM E408-71, reflectance from 5 to 40 microns at room temperature—
7Coating thickness range, Aeroglaze Z306 black polyurethane (NASA 2014 paper)Coating thickness range as printed in the table of coatings testedproduct Aeroglaze Z306, black polyurethane—
8Change in solar absorptance (delta alpha s), Z306 wake-positioned LDEF specimensRead from the paper's text on Z306 performance on LDEF (Figure 13); the paper says Z306 was otherwise optically stableplatform LDEF (Long Duration Exposure Facility), low Earth orbitposition wake positioned; specimens A0114 and A0138-6 as named in the textbasis change over the LDEF exposure, given as about -0.04 with the paper's Figure 13—
9Solar absorptance before LDEF EOIM III exposure, Chemglaze Z306 flight sample EOIM3-4-1 (NASA 1995 paper)Solar absorptance calculated from diffuse reflectance spectra after normalization to an NIST diffuse reflectance standard; the paper gives a measurement precision for this methodproduct Chemglaze Z306 black polyurethane paint, LDEF name; sample from the LDEF trailing edge with a contamination layerbasis dimensionless; the table prints no unit—
10Solar absorptance after LDEF EOIM III exposure, Chemglaze Z306 flight sample EOIM3-4-1 (NASA 1995 paper)Solar absorptance calculated from diffuse reflectance spectra after normalization to an NIST diffuse reflectance standardproduct Chemglaze Z306 black polyurethane paint, LDEF name; sample from the LDEF trailing edge with a contamination layerexposure EOIM III atomic oxygen test; the paper calls the change negligible and says the surface was erodedbasis dimensionless; the table prints no unit—
11Initial solar absorptance of the Z306 coating before LDEF M0003-8 exposure (NASA Boeing paper)Stated in the paper as the initial value; the measurement method is not printed in this paragraphproduct Chemglaze Z306 black polyurethane, applied to a graphite epoxy composite panel on LDEF experiment M0003-8basis dimensionless; the paper calls it the initial absorptance of the coating—
12Solar absorptance after LDEF M0003-8 exposure, Chemglaze Z306 (NASA Boeing paper)Measured on the exposed Z306 coated specimen; the method is not printed in this paragraphproduct Chemglaze Z306 black polyurethane on a graphite epoxy composite panel, LDEF experiment M0003-8 on tray D9exposure atomic oxygen and ultraviolet radiation as stated in the paper; the fluence and sun-hour figures are not copied herebasis dimensionless; the paper calls the drop from the initial value small and says the paint was otherwise little changed—
13Thermal emittance after LDEF M0003-8 exposure, Chemglaze Z306 (NASA Boeing paper)Measured on the exposed Z306 coated specimen; the method and angle are not printed in this paragraphproduct Chemglaze Z306 black polyurethane on a graphite epoxy composite panel, LDEF experiment M0003-8 on tray D9basis dimensionless; the paper attributes the higher value to the roughened, eroded surface—

Corrosion and compatibility

What happens when it meets other materials and environments.

Corrosion and compatibility
EnvironmentConcernWhat happens
Atomic oxygen in low Earth orbit, LDEF leading edge not rated On the LDEF leading edge, atomic oxygen roughened Z306 and raised its solar absorptance.1
Atomic oxygen, unprotected Z302 and Z306 polyurethane paints in low Earth orbit not rated Unprotected Z306 erodes at the polyurethane binder and the carbon pigment under atomic oxygen.2
Black-light illumination after LDEF exposure not rated After LDEF exposure, Z306 showed both stimulated and quenched fluorescence under black light.3
Moisture, hydrolysis of polyurethane in general not rated Polyurethanes in general may degrade by hydrolysis; no moisture-ageing test of Z306 was read.4
Light exposure in general, aromatic polyurethanes not rated Polyurethanes made with aromatic isocyanates contain chromophores that interact with light.5
Corrosion details
#EnvironmentDetailsTest conditions
1 Atomic oxygen in low Earth orbit, LDEF leading edge The LDEF A0034 interim results say that for Chemglaze Z306 coatings exposed on the leading edge, the results show increased coating roughness and, as a result, solar absorptance, from material erosion induced by atomic oxygen. Two Z306 specimens flew on the leading edge: one exposed through an open aperture (#01-44) and one under a sealed quartz window (#01-14). platform LDEF leading edge tray, low Earth orbitexposure LDEF mission; the exposure duration is not stated in the passage readspecimens #01-44 (open aperture) and #01-14 (sealed quartz window)
2 Atomic oxygen, unprotected Z302 and Z306 polyurethane paints in low Earth orbit The LDEF S0069 paper says Z302 and Z306, both polyurethane black paints, are susceptible to atomic-oxygen interactions that erode the polyurethane binder and the carbon pigment when they are not protected effectively. The same paper reports that Z306 was otherwise optically stable on LDEF. basis statement about both paints in the section heading; not a Z306-only erosion rate
3 Black-light illumination after LDEF exposure The LDEF A0034 paper says that S13G, S13G-LO and Z93 showed yellow colouration under black light that was quenched by space exposure, while the polyurethane paints A276 and Z306 showed both stimulated and quenched fluorescence after space exposure. YB-71 was not obviously affected. basis visual black-light observation in the paper; no fluorescence intensity was given
4 Moisture, hydrolysis of polyurethane in general Wikipedia states that polyurethanes may degrade due to hydrolysis. No Z306 moisture-ageing or humidity result was found in any source read for this profile. basis general statement about polyurethanes; not a Z306 test
5 Light exposure in general, aromatic polyurethanes Wikipedia states that polyurethanes, especially those made using aromatic isocyanates, contain chromophores that interact with light. The page does not say which isocyanate Z306 uses, so this is a general statement. basis general statement about polyurethanes; the Z306 isocyanate is not printed in any source read

Risks and side effects

Hazards to people, what happens when a cell overheats, and how the material is handled and stored.

For people

The Silmid page says the product contains diisocyanates with restrictions on supply and use in Great Britain, and Wikipedia states that isocyanates are skin and respiratory sensitizers.

Isocyanates
Silmid prints a diisocyanate restriction for Great Britain, and Wikipedia cites OSHA for skin and respiratory sensitization by isocyanates used in polyurethanes.
Transport
Silmid prints the transport entry UN Number 1263 CL3 for the 1 US gallon can.

If it fails

In orbit, the failure route in these sources is atomic oxygen erosion of the binder and the carbon pigment, measured on LDEF.

Atomic oxygen
On the LDEF leading edge, unprotected Z306 roughened and its solar absorptance rose, per the A0034 interim results. The S0069 paper says the binder and carbon pigment erode when they are not protected effectively.
Wake positions
Two wake-positioned LDEF specimens, A0114 and A0138-6, showed a change in solar absorptance of about -0.04, per the S0069 paper.

Test details
The original wording and numbers from the sources, for readers who want them.

Failure risks

Failure risks
FailureTrigger and consequence
Atomic oxygen erosion of the binder and carbon pigmentmoderate severityUnprotected exposure to atomic oxygen in low Earth orbit, as on the LDEF leading edgeIncreased roughness and a rise in solar absorptance on the leading edge, per the LDEF A0034 interim results; the LDEF S0069 paper says protection is needed.
Small drop in solar absorptance on wake-positioned surfaceslow severityExposure in the wake position on LDEF, as on specimens A0114 and A0138-6A change in solar absorptance of about -0.04, per the LDEF S0069 paper and its Figure 13.

Handling and storage

  • The Silmid product page offers a technical data sheet and a safety data sheet only after login. Their content was not read, so no handling step is recorded from a manufacturer or SDS source.

Mitigations

  • The LDEF S0069 paper reports silicone overcoats on Z302 that showed little change in solar absorptance, but it does not test an overcoat on Z306.

Supply and geography

How common the raw materials are and where they come from.

Manufacturer and distribution

Updated