Thermal conductivity
The thermal finishing configuration selector allows you to quickly obtain a selection of thermal finishing solutions suitable for your project. However, do not hesitate to contact us using our contact form to obtain the advice of our experts.
MAPSIL® QS 1123 ELEC LD
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Technical sheet | |
| Introduction | Low outgassing, Silicone-2K, electrically and thermally conductive adhesive. MAPSIL QS1123 ELEC LD is an adhesive elastomer, designed to participate in the passive electrical and thermal regulation of satellites during their missions. This coating is specifically adapted to withstand the aggressions of the space environment and thus guarantee its function over a long service life. This coating meets various environmental and strategic regulations, but also the quality requirements of EN9100 and space companies. It has a significant number of characterisations, publications and flight references. This coating is Ground & Flight" rated on many substrates, notably through the fine tuning of special procedures we develop. | |
| Usages | MAPSIL® QS 1123 ELEC LD is a silicone adhesive elastomer for bonding applications including OSR bonding. | |
| Advantages | -ITAR / EAR Free Products -REACH Compliant Products | |
| Associated services | - Coating application service possible (MAP SPACE COATINGS premises or Customers premises / please contact us) - Thermo-optical, mechanical, thermal, rheological, outgassing, electrical, thermo-mechanical Expertise / Characterisation - Training in the implementation of coatings - Application audit | |
| Quality | - ISO 9001 - EN 9100 - ASF CNES - Systematic checking of all batches - Characterisations carried out as defined on the statement of conformity | |
| Solar absorptivity | NA | |
| Infrared emissivity | NA | |
| Electrical resistance | 3x10^5 Ohm/² | |
| Thermal conductivity | 0.36 W.m^-1.K^-1 (CNES) 0.25 W.m^-1.K^-1 (ASTM C177) | |
| Ultimate tensile strength | 3.1 MPa | |
| Elongation at rupture | 80% | |
| Shore A hardness | 74 | |
| RML | 0,27% | |
| CVCM | 0,04% | |
| Substrates | GLASS - COMPOSITES - METAL ALLOYS | |
| Primer | ALU D - PSX | |
| Qualification report reference | DCT/TV/TH-2011-8705_Test_ESD Thermal conductivity measurementDCT-TV-TH-2012-5586 EIGHT YEARS GEO GROUND TESTING OF THERMAL CONTROL COATINGS_DCT/TV/TH/NT10-1267 QUALIFICATION REPORT MAPSIL-QS1123-DCT-TV-THNT09-14628 QUALIFICATION REPORT EIGHT YEARS GEO GROUND SIMULATION N/S FACES ON ANTISTATIC PIGMENT RF2/14062 DESP MAPSIL QS1123 ELEC LD_DCT-TV-TH 2013-2456 | |
| Satellite reference | . | |
| TIS | . | |
| Product family | Adhesives | |
| Ageing properties | Tested in: - Geo Env - Ground storage - ESD | |
MAPSIL® 210
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Technical sheet | |
| Introduction | Low-outgassing thermal silicone grease for satellites. MAPSIL® 210 is a thermal satellite grease, designed to participate in the passive thermal regulation of satellites during their missions. This coating meets various environmental and strategic regulations, but also the quality requirements of EN9100 and space companies. | |
| Usages | MAPSIL® 210 is a silicone grease with high thermal conductivity for the production of thermal joints. | |
| Advantages | -ITAR / EAR Free Products -REACH Compliant Products | |
| Associated services | - Thermal, rheological, outgassing expertise / characterisation | |
| Quality | - ISO 9001 - EN 9100 - 100% checking of batches - Characterisations carried out as defined on the statement of conformity | |
| Solar absorptivity | NA | |
| Infrared emissivity | NA | |
| Electrical resistance | NA | |
| Thermal conductivity | NA | |
| Ultimate tensile strength | NA | |
| Elongation at rupture | NA | |
| Shore A hardness | NA | |
| RML | NA | |
| CVCM | NA | |
| Substrates | . | |
| Primer | NA | |
| Qualification report reference | QUALIFICATION REPORT _89_CT_DRT_TVE_TH_074 | |
| Satellite reference | . | |
| TIS | . | |
| Product family | Lubricants | |
| Ageing properties | . | |
MASTIC AS
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Technical sheet | |
| Introduction | Thermal and anti-static silicone finish coating for launcher. MASTIC AS is used to withstand the launch pad environment and stresses during launch. These two environments can degrade the launchers efficacy and reliability. MASTIC AS thus reduces the risk of corrosion, overheating and static electric discharge due to air friction, on launch. This coating meets various environmental and strategic regulations, but also the quality requirements of EN9100 and space companies. It has a significant number of characterisations, publications and flight references. This coating is Ground & Flight" rated on many substrates. | |
| Usages | MASTIC AS coating is used on several parts of the launcher, especially on parts coated with silicone thermal protection (upper part of the boosters, etc.). | |
| Advantages | -ITAR / EAR Free Products -REACH Compliant Products -Repair kit -Stripping kit | |
| Associated services | - Thermo-optical, mechanical, thermal, rheological, outgassing, electrical, thermo-mechanical Expertise / Characterisation - Training in the implementation of coatings - Application audit | |
| Quality | - ISO 9001 - EN 9100 - 100% checking of batches - Characterisations carried out as defined on the statement of conformity | |
| Solar absorptivity | 0,42 | |
| Infrared emissivity | 0,85 | |
| Electrical resistance | 1-1000x10^6 Ohm/² | |
| Thermal conductivity | NA | |
| Ultimate tensile strength | NA | |
| Elongation at rupture | NA | |
| Shore A hardness | NA | |
| RML | NA | |
| CVCM | NA | |
| Substrates | Silicone-based materials: Prosial® LS - Prosial® 2000 Cork P50 Aluminium 7075T0 Glass | |
| Primer | . | |
| Qualification report reference | Thermal cycling_MASTIC-AS-DTS-AE-MTE-TH-02-061 Surface electrical resistance_MASTIC-AS-CT-DRT-TVE-TH-328 Thermo-optical properties_MASTIC-AS-CT-DRT-TVE-TH-591 | |
| Satellite reference | Ariane V, VEGA launchers | |
| TIS | . | |
| Product family | Launcher Coatings | |
| Ageing properties | Tested in: - Ground storage (cold, heat, salt spray, thermal shock, etc.) | |
MAPATOX 41-B
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Technical sheet | |
| Introduction | Low-outgassing, transparent Silicone-2K coating MAPATOX 41-B is a silicone coating designed to help protect satellite substrates from atomic oxygen. This coating is specifically adapted to withstand the aggressions of the space environment and thus guarantee its function over a long service life. This coating meets various environmental and strategic regulations, but also the quality requirements of EN9100 and space companies. It has a significant number of characterisations, publications and flight references. | |
| Usages | MAP ATOX 41-B is a silicone varnish used to protect materials that are sensitive to the action of atomic oxygen (Kapton, Mylar, Composites, etc.). MAP ATOX 41-B provides a perfectly transparent optical film and an absence of corrosion in the presence of some components (KOVAR). | |
| Advantages | -ITAR / EAR Free Products -REACH Compliant Products | |
| Associated services | - Coating application service possible (MAP SPACE COATINGS premises or Customers premises / please contact us) - Thermo-optical, mechanical, thermal, rheological, outgassing, electrical, thermo-mechanical Expertise / Characterisation - Training in the implementation of coatings - Application audit | |
| Quality | - ISO 9001 - EN 9100 - 100% checking of batches - Characterisations carried out as defined on the statement of conformity | |
| Solar absorptivity | NA | |
| Infrared emissivity | NA | |
| Electrical resistance | > 10^12 Ohm/² | |
| Thermal conductivity | 0.15 W.m^-1.K^-1 | |
| Ultimate tensile strength | . | |
| Elongation at rupture | . | |
| Shore A hardness | 43 | |
| RML | 0,45% | |
| CVCM | 0,05% | |
| Substrates | KAPTON - MYLAR - COMPOSITE | |
| Primer | PSX | |
| Qualification report reference | QUALIFICATION REPORT _89_CT_DRT_TVE_TH_074 DT_96_090_DGA_T_AE_MTE_TH DCT_TV_TH_2012_13180 QUALIFICATION MAPATOX-41B ON KAPTON HN _ DSO TB TH 2017 18795 | |
| Satellite reference | . | |
| TIS | . | |
| Product family | Silicone Conformal Coatings | |
| Ageing properties | Tested in: - Geo Env - LEO Env - Ground storage - ATOX - ESD | |
MAP® AQ STATIC
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Technical sheet | |
| Introduction | Waterborne, thermal and anti-static polyurethane finish coating for launcher. MAP AQ STATIC is used to withstand the launch pad environment and stresses during launch. These two environments can degrade the launchers efficacy and reliability. MAP AQ STATIC thus reduces the risk of corrosion, overheating and static electric discharge due to air friction, on launch. This coating meets various environmental and strategic regulations, but also the quality requirements of EN9100 and space companies. It has a significant number of characterisations, publications and flight references. This coating is Ground & Flight" rated on many substrates. | |
| Usages | MAP AQ STATIC coating can be applied to certain parts of the launcher, in composite and metallic alloys such as: Cryogenic main stage Acceleration stages with powder or boosters | |
| Advantages | -ITAR / EAR Free Products -REACH Compliant Products -Repair kit -Stripping kit | |
| Associated services | - Thermo-optical, mechanical, thermal, rheological, outgassing, electrical, thermo-mechanical Expertise / Characterisation - Training in the implementation of coatings - Application audit | |
| Quality | - ISO 9001 - EN 9100 - 100% checking of batches - Characterisations carried out as defined on the statement of conformity | |
| Solar absorptivity | 0,3 | |
| Infrared emissivity | 0,9 | |
| Electrical resistance | 10^5 - 10^9 Ohm/² | |
| Thermal conductivity | NA | |
| Ultimate tensile strength | NA | |
| Elongation at rupture | NA | |
| Shore A hardness | NA | |
| RML | NA | |
| CVCM | NA | |
| Substrates | Cork, foam, composite, metal, glass substrates: CFRP - NORCOAT HPK - Cryosof 2 - H920A - Cork P50 - Aluminium 7075T0 - Glass | |
| Primer | E - MAP®AQ PRIMER - MAPSIL® SILICo + E | |
| Qualification report reference | QUALIFICATION REPORT DCT-TV-TH-NT11-4384 | |
| Satellite reference | Ariane V, VEGA launchers | |
| TIS | . | |
| Product family | Launcher Coatings | |
| Ageing properties | Tested as per: -A5-SG-1-X-30-ASAI: General design specification for on-board electrical systems -VG-SG-1-C-0035-SYS: General design norms and rules -A5-SG-1-X-40-ASAI: Qualification and acceptance in environment specification for equipment | |
MAP® PU1
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Technical sheet | |
| Introduction | Low-outgassing black polyurethane thermal control coating for satellites PU1 is a thermal finishing coating for satellites, designed to participate in the passive thermal regulation of satellites during their missions. This coating is specifically adapted to withstand the aggressions of the space environment and thus guarantee its function over a long service life. This coating meets various environmental and strategic regulations, but also the quality requirements of EN9100 and space companies. It has a significant number of characterisations, publications and flight references. This coating is Ground & Flight" rated on many substrates, notably through the fine tuning of special procedures we develop. | |
| Usages | PU1 thermal finish is especially used to ensure passive thermal regulation on: Antennas Circulators Protections Electronic boxes Thermal vacuum chambers MLI OMUX Optical baffles Optical parts Panels RF equipment Wave guides | |
| Advantages | -ITAR / EAR Free Products -REACH Compliant Products -Product qualified FAST CURING Process -Repair kit -Stripping kit | |
| Associated services | - Coating application service possible (MAP SPACE COATINGS premises or Customers premises / please contact us) - Thermo-optical, mechanical, thermal, rheological, outgassing, electrical, thermo-mechanical Expertise / Characterisation - Training in the implementation of coatings - Application audit | |
| Quality | - ISO 9001 - EN 9100 - ASF CNES - Systematic checking of all batches - Characterisations carried out as defined on the statement of conformity | |
| Solar absorptivity | 0,96 | |
| Infrared emissivity | 0,88 | |
| Electrical resistance | >10^12 Ohm/² | |
| Thermal conductivity | NA | |
| Ultimate tensile strength | NA | |
| Elongation at rupture | NA | |
| Shore A hardness | NA | |
| RML | 0,39% | |
| CVCM | 0,04% | |
| Substrates | ALODINE ALU - GOLD-PLATED ALU - ALU 2017T4 CFRP Kapton STAINLESS STEEL - INVAR Fe36Ni - TITANIUM TA6V - SILVER ALU - CFRP IM7/6-8552 - Kapton ALU 25 µm Kapton FACE- Kapton ALU 25 µm ALU FACE - MYLAR ALU 25 µm Mylar FACE- MYLAR ALU 25 µm ALU FACE- ALU AU4G ALAL ALALALAG AL AL AL STAINLESS STEEL AL AG ALD NI ALAG TI CU ALCOA AL AL ALD ALD INVAR - INVAR 36 - AL 6082T6 AL STAINLESS STEEL - TA6V - AL 1050 CU STAINLESS - AL SURTEC 650 - SmCO MAGNET - TREATED STAINLESS STEEL SULFINERT - STAINLESS STEEL 304L | |
| Primer | E' - PH11 - PSX PS - PH11 + E' - MAPSIL SILICo + E' | |
| Qualification report reference | EXTENSION OF SHELF LIFE_ DCT-TV-TH-2013-0001178 Fast Curing DCT-TV-TH-2014-10593 Additional qualification report DCT-TV-TH-NT11-3938 Additional qualification report DCT/TV/TH/NT08-5073 Additional qualification report DCT-TV-TH-04-626 THERMAL CYCLING AFTER ACCELERATED CURING_NT-99-016/DTS/AE/MTE/TH MOISTURE TEST THERMAL CYCLING UNDER VACUUM-OUTGASSING SURFACE POTENTIAL_ 88/CT/DRT/TVE/TH n°411 SPECTRAL MEASUREMENT @ CRYOGENIC TEMPERATURE_NT100/CT/AE/MTE/TH | |
| Satellite reference | SPOT 2 SPOT 4 TELECOM 2 PRONAOS HELIOS SCARAB TURKSAT INTELSAT VII DEMETER SYRACUSE 3B THEOS GALAXY 17 ARABSAT 4 PICARD SPIRALE AEOLUS ALADIN ROCSAT 2 SKYNET 5 CHINASAT AMOS 3 GOSAT CIEL 2 AMAZONAS KAZAKHSTAN YAMAL 402 | |
| TIS | . | |
| Product family | Thermal Control coatings for Satellites | |
| Ageing properties | Tested in: - Satellite internal environment - ESD | |
