| Data still to be completed------(<---links) | |
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| PRODUCT DATA of Solithane 113/C 113-300 (100/73 pbw) |
| Material | Solithane 113/C 113-300 (100/73 pbw) |
| Product Type | Two-part, soft, transparent, potting, conformal coating, bonding agent. |
| Chemical Composition | Polyurethane |
| Name of Manufacturer | Uniroyal Chemical Company Inc
(Crompton Corporation), 214 West Ruby Avenue,, Gastonia NC 28053, USA +1 704 864-3411 +1 704 864-4079 bob_marionneaux@cromptoncorp.com www.cromptoncorp.com |
| EXPERIENCE IN PRACTICE |
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| Development Status | Commercial Product |
| Cost Range | Low |
| Lot Reproducibility | Excellent |
| Space Experience | Extensive |
| PHYSICAL PROPERTIES |
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| Specific Gravity | 1.07 |
| Viscosity | 20000 cP @ 27°C |
| Pot Life | 180 min @ 27°C |
| ELASTIC PROPERTIES |
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| Tensile Modulus | 0.004 GPa Remark:Room temperature data from Cryogenics 48 (2008) 497-510 Data Quality: Limited Laboratory testing |
| ELECTRICAL PROPERTIES |
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| Electrical Volume Resistivity | 2.5e12 ohm.m @ 27°C |
| Dielectric Constant | 4.2 @ 27°C, 1kHz |
| Dielectric Strength | 14.9 @ 27°C |
| Dissipation Factor | 0.162 @ 27°C, 1kHz |
| THERMAL PROPERTIES |
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| Thermal Expansion Coefficient | 238 μstrain/°C Remark: 0°C to 70°C 126 x 10-6 /°C for -55°C to -15°C |
| Glass Transition Temperature | -10 °C Remark: Thermal expansion measurement |
| RELEVANT PROPERTIES FOR USE IN SPACE COMMUNITY |
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| Flammability | Fail (21% O2) Test: NASA NHB 8060-1B |
| Thermal Cycling | Pass Test: ECSS-Q-70-04 |
| Temperature Range(space) | -60°C to 120°C max. Test: Long Term |
| Outgassing | TML = 0.37%, RML =0.21%, CVCM = 0.01% Test: ECSS-Q-70-02 |
| Oxygen Index | 24.7 Test: ECSS-Q-70-21 |
| SPECIAL RECOMMENDATIONS |
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| Special Recommendations | Recommended cures: 7 days at room temperature, or 24 hours at 70°C. · Compositions other than the one detailed here are possible. Large amounts of experimental data on them exists and is available on demand. · Not resistant to solar UV radiation. · Owing to flammability risk, not to be used as a conformal coating in manned spacecraft unless a fire-resistant overcoating is used. It’s acceptability as an adhesive will depend on the configuration. · Possible use as a screw-locking compound. · Possible use as an ink with suitable addition of pigments and solvents. · Possible use as a conductive coating when filled with silver powder. · Flammability highly dependent on coating thickness. Configuration flammability tests required. |