NewSpace Market · Sector Catalogue
Thermal Control
Every unit we list in this sector — specifications, manufacturers and where to ask for a quote. Compiled from the live NewSpace Market catalogue.
About this catalogue
What is inside
This catalogue lists 111 thermal control products offered by 27 manufacturers across 9 countries. Of those, 50 carry a manufacturer datasheet and 1 publish a price; the rest are quoted on request — normal in this market, where configuration drives cost.
Entries are grouped alphabetically by manufacturer. Every product links back to its page on newspacemarket.com, where you will find the full specification, the datasheet and a quote form that reaches the manufacturer directly.
Compiled 26 August 2026 from the live catalogue. Specifications are as published by the manufacturers; we normalise units but do not re-measure. Where a figure looked implausible it was left out rather than guessed.
Manufacturers by country
Overview
All products at a glance
| Product | Manufacturer | Country | Key specification | Price |
|---|---|---|---|---|
| 4C-PURE™ Cabled Copper Thermal Straps | Thermal Space Ltd. | United States | Material: OFHC Copper (C101, C10100), 99.99% purity | on request |
| Absolute Pressure Sensor Vt 220 | Glavkosmos | Russia | Range of measurements: 0-0.125; 0-0.250; 0-0.500 | on request |
| Acusil® Thermal Protection System (TPS) | Peraton Space | United States | Acusil® ii ablation resistance: zero ablation in heat fluxes up to 100 W/cm2 | on request |
| Aerospace Tape (Spacecraft Thermal Control Tape) | DUNMORE | United States | Variants: Second Surface Aluminized Kapton Tape, Stamet Coated Black Kapton… | on request |
| Aerospace Thermal Control Materials | Sheldahl (Multek Flexible Circuits) | United States | Flight heritage: Space thermal control material heritage since 1958 | on request |
| All-Polyimide (KAPTON®) Heaters | Minco Products, Inc | United States | Maximum operating temperature: 260°C | on request |
| Altom10 Series — LHP Evaporator Modules for Microelectronics | Allatherm | Latvia | Materials: Copper (Cu) and Stainless Steel (SS) | on request |
| Altom14 Series — LHP Evaporator Modules for Power Electronics | Allatherm | Latvia | Material: Stainless Steel (SS) | on request |
| Arterial Heat Pipes | Glavkosmos | Russia | Purpose: Thermal control of spacecraft equipment. | on request |
| AstraWrap™ HT | Aerospace Fabrication and Materials, LLC | United States | Standard material width: 48 inches | on request |
| AstraWrap™ Thermal Insulation Space Wrap | Aerospace Fabrication and Materials, LLC | United States | Film Thickness: 0.25 mil (6 µm) | on request |
| Axial Grooved Heat Pipes | Glavkosmos | Russia | Purpose: Thermal control of spacecraft equipment | on request |
| Axial, Arterial, Contour Heat Pipes, Radiator Heat Pipe | Glavkosmos | Russia | Purpose: Design and manufacture of products for providing thermal regime wi… | on request |
| Conductive Glass Fabric High-Temperature Vacuum Insulation | RUAG Space | Switzerland | Maximum temperature: Up to 550 degrees C | on request |
| Constant Conductance Heat Pipes (CCHPs) | ACT (Advanced Cooling Technologies) | United States | Space flight hours heritage: 118,664,340+ hours | on request |
| Contour Heat Pipes | Glavkosmos | Russia | Purpose: Thermal control of spacecraft equipment. | on request |
| Control unit of the thermal regime support system | SPUTNIX | Russia | Dimensions: 200 x 130 x 30 mm | on request |
| Controllers | Minco Products, Inc | United States | Operating temperature: -50 to 260 °C | on request |
| COOLCAT Cryogenic Superinsulation | RUAG Space | Switzerland | Coolcat 2 nw: 10 layers double-sided aluminized perforated polyester foil i… | on request |
| Copper Cable Thermal Straps (CuTS) | Technology Applications Inc (TAI) | United States | Material: 99.99 - 99.998% pure OFHC copper (Cu-101) | on request |
| Cryocooler Series Thermal Straps (CS-CuTS) | Technology Applications Inc (TAI) | United States | Material: 99.99 - 99.998% pure OFHC copper (Cu-101) | on request |
| Cryocoolers | Northrop Grumman Space Systems | United States | On-orbit operation: More than 300 combined years | on request |
| Cryogenic Cabling | Aerospace Fabrication and Materials, LLC | United States | — | on request |
| Cryogenic Multilayer Superinsulation | Aerospace Fabrication and Materials, LLC | United States | Operating temperature: below -100 °C | on request |
| Cryogenic Tanks | Aerospace Fabrication and Materials, LLC | United States | — | on request |
| Custom Cold Plates | Thermal Space Ltd. | United States | Materials: Copper, aluminum, AlSiC, graphite | on request |
| Custom Soft Goods Manufacturing | Aerospace Fabrication and Materials, LLC | United States | — | on request |
| Deployable Radiators for Satellites | Arquimea | Spain | Architecture: Multi-Loop Heat Pipes (LHP) with embedded condenser lines | on request |
| DUN-COOL Thermal Management Film | DUNMORE | United States | Function: Radiator or optical solar reflector (OSR) | on request |
| DUN-DIFFUSE White Kapton Polyimide Film | DUNMORE | United States | Base film: 100 Ga (25 micron) | on request |
| Electric Heaters | Glavkosmos | Russia | Purpose: Designed to provide thermal conditions for spacecraft onboard equi… | on request |
| Electric Heaters for Manned Spacecraft | Glavkosmos | Russia | Year of release: 2015 | on request |
| Elements | Minco Products, Inc | United States | Temperature range: -50 to 260 °C | on request |
| Flexible Thermal Protection for Launchers | RUAG Space | Switzerland | Maximum temperature: Up to 1500 degrees C | on request |
| Flexible Thermal Straps | Lidax | Spain | Materials: High Thermal Conductivity Materials (Copper, Pyrolytic Graphite) | on request |
| Gas Thermal Compressor | Allatherm | Latvia | Gases handled: Krypton, Xenon, Hydrogen, hydrocarbons | on request |
| GPU on Diamond | Akash Systems | United States | — | on request |
| Graphite Fiber Thermal Straps (GFTS) | Technology Applications Inc (TAI) | United States | Fiber material: GraFlex I / II carbon-fiber bundles; GraFlex III woven grap… | on request |
| Heat Pipes (HP) | Calyos | Belgium | Technology: Latent heat of vaporization, wick return | on request |
| Heat Pipes for Space Applications (Axial, Arterial, Diode) | Arquimea | Spain | Heat pipe types: Axial grooved, arterial, diode | on request |
| High Performance Radiator technology (HiPeR) Flexlinks | Airbus Defence and Space | France | Conductance-to-mass ratio: three to five times higher than traditional solu… | on request |
| High Temperature Plume Shields | Aerospace Fabrication and Materials, LLC | United States | Temperature Range: 300C to 1,000C and above | on request |
| High-Temperature Heat Pipes | ACT (Advanced Cooling Technologies) | United States | Potassium operating range: 400–1,000°C | on request |
| HiK Plates / Heat Pipe Assemblies | ACT (Advanced Cooling Technologies) | United States | Operating temperature range: 20–150°C | on request |
| Honeycomb Radiator Panels | ACT (Advanced Cooling Technologies) | United States | Core material: Aluminum honeycomb sandwich | on request |
| Humidity Sensors | Minco Products, Inc | United States | Operating temperature: -50 to 260°C | on request |
| IberEspacio Satellite Thermal Control Hardware | Arquimea | Spain | Heat transfer capacity (LHP): Up to 1 kW standard; >1.2 kW multi-evaporator | on request |
| k-Core Encapsulated Graphite Thermal Solutions | Boyd Corporation | United States | Effective thermal conductivity (k-Core assembly): up to 1000 W/m·K | on request |
| Loop Heat Pipes (LHP) | Calyos | Belgium | Power vs. water-based cooling: Up to 100% less | on request |
| Loop Heat Pipes (LHPs) | ACT (Advanced Cooling Technologies) | United States | Ammonia operating range: -40°C to 70°C | on request |
| Loop Heat Pipes for Space Applications | Arquimea | Spain | Heat transfer power: Up to 1 kW | on request |
| Low Temperature Heat Pipes | Glavkosmos | Russia | Purpose: Aggregate of systems for ensuring the thermal regime of the spacec… | on request |
| LPT 9310 HP COTS+ | Thales Cryogenics | Netherlands | Cooling capacity: 5.7 W | on request |
| LPT 9510 COTS+ | Thales Cryogenics | Netherlands | Cooling capacity: 1.4 W at 80 K | on request |
| LPT6510 Pulse-tube Cryocooler | Thales Cryogenics | Netherlands | Max input: 60 W (AC); higher-power versions on request | on request |
| MAP SPACE COATINGS (Company Profile) | MAP (Aerospace Coatings) | — | Color: White | on request |
| MAP SPACE COATINGS Thermal Finishing Services | MAP (Aerospace Coatings) | — | Coating type: Water-based, silver-loaded polyurethane | on request |
| Mica THERMOFOIL TM Heaters | Minco Products, Inc | United States | Watt Density: up to 110 W/in² | on request |
| Micro Channel Heat Pipes (MCHP) | Calyos | Belgium | Design: Flat aluminium, customizable length and bends | on request |
| Miniature Sensors | Minco Products, Inc | United States | Temperature range: -50 to 260 °C | on request |
| MLI | Hemeria | France | — | on request |
| MLI Blankets | DHV Technology | Spain | — | on request |
| MMOD Shields | Aerospace Fabrication and Materials, LLC | United States | — | on request |
| Multi-Layer Insulation | DUNMORE | United States | — | on request |
| Multi-layer Insulation Blankets | DHV Technology | Spain | — | on request |
| Multilayer Insulation Blankets | Aerospace Fabrication and Materials, LLC | United States | Operating temperature: -250…+1300 °C | on request |
| OHP Radiators | Thermavant | United States | Simple radiator example thermal performance (OHP): 2 °C rise per 150 W | on request |
| Phase Change Material (PCM) Heat Sinks | ACT (Advanced Cooling Technologies) | United States | Thermal storage advantage: 1–2 orders of magnitude higher than sensible ene… | on request |
| PolaLam | Aerospace Fabrication and Materials, LLC | United States | Spacer layer thickness: 5.0 mil | on request |
| PolaPair™ | Aerospace Fabrication and Materials, LLC | United States | Standard Lengths: 100, 200, and 500 feet | on request |
| PolaTape™ | Aerospace Fabrication and Materials, LLC | United States | Material: Polyester-based aluminized reflective tape | on request |
| PolaWrap™ | Aerospace Fabrication and Materials, LLC | United States | Reflector separation spacer thickness: 5.0 mil (127 µm) | on request |
| Polyimide (Kapton®) Thermofoil™ Heaters | Minco Products, Inc | United States | Mass: 0.009 oz/in² | on request |
| Probes & Probe Assemblies | Minco Products, Inc | United States | Temperature range: -50 to 260 °C | on request |
| PSG Thermal Links (Pyrolytic Graphite Flexible Thermal Straps) | Lidax | Spain | Material: Pyrolytic Graphite Sheet (PGS) | on request |
| PTFE (Teflon) Heaters | Minco Products, Inc | United States | Operating temperature: -200 to 150°C | on request |
| Pulsating Heat Pipes (PHP) | Calyos | Belgium | Php spreader dissipation: 800 W | on request |
| Pulsating Heat Pipes (PHPs) | ACT (Advanced Cooling Technologies) | United States | Wick structure: None (wickless) | on request |
| PyroFlex PGS & Graphene Thermal Straps (X-Series) | Technology Applications Inc (TAI) | United States | Material: Pyrolytic Graphite Film/Sheet (PGF/PGS), optional Graphene Layere… | on request |
| Radiation Refrigerator | Glavkosmos | Russia | Year of release: 2003 | on request |
| Radiators | Aerospace Fabrication and Materials, LLC | United States | — | on request |
| Satellite Multi-Layer Insulation (MLI) | RUAG Space | Switzerland | Operating temperature: 1 K to 1800 K | on request |
| Satkit MLI Satellite Kit | DUNMORE | United States | Kit contents: Outer layer material roll, inner layer material roll, polyimi… | on request |
| Screen-Vacuum Thermal Insulation of Orbital Spacecraft | Glavkosmos | Russia | Flight qualification of the product: Yes | on request |
| Silicone Rubber Heaters | Minco Products, Inc | United States | Operating temperature: -45 to 235 °C | on request |
| SmartHeat™ SLT Thin-Film Heaters | Minco Products, Inc | United States | Temperature range: -45°C (-49°F) to 100°C (212°F) | on request |
| Space Copper-Water Heat Pipes (SCWHPs) | ACT (Advanced Cooling Technologies) | United States | Heat flux capability: Up to 50 W/cm² | on request |
| Space Liquid Cooling Systems | ACT (Advanced Cooling Technologies) | United States | Cooling type: Single-phase liquid (pumped fluid loop) | on request |
| Spacecraft Components | Aerospace Fabrication and Materials, LLC | United States | — | on request |
| Spacecraft Thermal Management Systems | Boyd Corporation | United States | Products: Heat pipes (CCHP/VCHP), vapor chambers, thermal straps, thermal i… | on request |
| Specialty Materials | Aerospace Fabrication and Materials, LLC | United States | PolaWrap Length: 10 feet | on request |
| SR630 Thermocouple Monitor Replacement Thermal Shield | Pumpkin, Inc. | United States | — | $64.95 |
| Stator Sensors | Minco Products, Inc | United States | Operating temperature: -50 to 260°C (-58 to 500°F) | on request |
| Sun Shields | Aerospace Fabrication and Materials, LLC | United States | Dimensions: up to 3 meters | on request |
| Surface Sensors | Minco Products, Inc | United States | Temperature range: -50 to 260 °C | on request |
| SX-SBOX Thermal Control (Microsatellite) | SPUTNIX | Russia | Thermal control unit sx-sbox-thermu-01: 200 × 130 × 30 mm, 600 g, ≤5 W (hea… | on request |
| Temperature Sensors | Minco Products, Inc | United States | Thermocouples Temperature Range: -200°C to 2300°C | on request |
| Temperature-controlled Honeycomb Panel | Glavkosmos | Russia | Flight qualification of the product: Yes | on request |
| Thermal and Structural Subassemblies for Space | Arquimea | Spain | Subsystem types: Laser terminal thermal systems, spacecraft modular thermal… | on request |
| Thermal Blankets for Space Applications (MLI) | Arquimea | Spain | Mli types: Standard plastic MLI, sewn fabric coated MLI, external MLI, inte… | on request |
| Thermal Control Unit | CAVU Aerospace | United Kingdom | Dimensions (L×W×H): 160 mm × 170 mm × 38 mm | on request |
| Thermal LyNX® | Thermal Space Ltd. | United States | Thermal conductivity-to-mass ratio: ~2x better than other thermal strap types | on request |
| Thermal-Clear TM Transparent Heaters | Minco Products, Inc | United States | — | on request |
| Thermal-Protection Materials for Spacecraft | Glavkosmos | Russia | Purpose: Provision of normal thermal conditions on passing the dense atmosp… | on request |
| Thermally Conductive Vibration Isolation System (TCVIS) | Technology Applications Inc (TAI) | United States | Function: Combined thermal transport (via GFTS graphite fiber strap) and 6-… | on request |
| Thermo-Modulating Heat Pipes (TMHPs) | ACT (Advanced Cooling Technologies) | United States | Working fluid / envelope: Aluminum-ammonia | on request |
| Thermo-Structural Radiator Panels for Space | Arquimea | Spain | Panel materials: Aluminum skins + aluminum honeycomb core | on request |
| Thin Metal Foil Thermal Straps (TMF Series™) | Thermal Space Ltd. | United States | Copper type/purity: Electrical Tough Pitch (ETP), C110/99.9% | on request |
| Vapor Chambers | ACT (Advanced Cooling Technologies) | United States | Standard planar dimensions: Up to 10" × 20" | on request |
| Variable Conductance Heat Pipes (VCHPs) | ACT (Advanced Cooling Technologies) | United States | Effective thermal conductivity: 10,000 to 100,000 W/m·K | on request |
| xRAD™ Extruded Thermal Control Radiator | Paragon Space Development Corporation | United States | Technology: Extruded aluminum panels with integral coolant channels (patented) | on request |
Products
Products by manufacturer
ACT (Advanced Cooling Technologies)
United States · 2003 · 12 productsPremier thermal management solutions company specializing in custom two-phase heat transfer technology for aerospace, defense, and industrial applications.

Constant Conductance Heat Pipes (CCHPs)
Precision-engineered aerospace CCHPs with over 118 million space flight hours heritage, manufactured under ISO 9001:2015 and AS9100D certified quality systems.
| Space flight hours heritage | 118,664,340+ hours |
| Quality certification | ISO 9001:2015, AS9100D |
| Welding standard | AWS D17.1 |
| Leak detection method | Helium mass spectrometer |
| Fluid purity process | Triple distillation |

High-Temperature Heat Pipes
Alkali metal heat pipes operating from 400°C to 1,100°C using potassium, NaK, or sodium in stainless steel or Haynes envelopes for nuclear space power, solar thermal, and hypersoni
| Potassium operating range | 400–1,000°C |
| Nak operating range | 500–800°C |
| Sodium operating range | 500–1,100°C |
| Envelope materials | Stainless Steel, Inconel Alloy 600, Haynes |
| Ifl temperature uniformity | ±0.1°C |

HiK Plates / Heat Pipe Assemblies
Custom heat spreaders with embedded copper-water heat pipes offering effective thermal conductivities of 10,000–100,000 W/m·K, designed to collect and move heat from multiple compo
| Operating temperature range | 20–150°C |
| Effective thermal conductivity | 10,000–100,000 W/m·K |
| Outer diameter range | 1/16" (1.5 mm) to 1.5" (38 mm) |
| Cross-section geometry | Round, rectangular, or flattened |
| Surface coating options | Nickel or tin |

Honeycomb Radiator Panels
Aluminum honeycomb sandwich panels serving dual roles as spacecraft structural shells and heat rejection radiators, with embedded CCHPs, high-conductivity face sheets, and selectab
| Core material | Aluminum honeycomb sandwich |
| Face sheet enhancement | High-conductivity, optional embedded CCHPs |
| Surface finish | Selectable emissivity coatings |
| Compatible orbit classes | LEO, MEO, GEO, deep space |
| Scalability | CubeSat-class to GEO bus panels |

Loop Heat Pipes (LHPs)
High-capacity two-phase heat transport devices that move larger amounts of heat over longer distances than conventional heat pipes, with sintered nickel, hybrid, and 3D-printed wic
| Ammonia operating range | -40°C to 70°C |
| Titanium/water variant range | 70°C to 250°C |
| Traditional wick pore radius | ~1 µm |
| 3d-printed wick pore radius | ~8–10 µm |
| 3d-printed wick TRL | 6 |

Phase Change Material (PCM) Heat Sinks
High-performance PCM thermal energy storage devices that absorb pulsed or duty-cycled heat loads with minimal temperature rise, for single and two-phase liquid cooling loops.
| Thermal storage advantage | 1–2 orders of magnitude higher than sensible energy storage |
| Typical pcm thermal conductivity (paraffin) | < 1 W/m·K |
| Enhancement structures | Fins, embedded heat pipes, metal foams |
| Manufacturing | Aluminum vacuum brazing, hermetic sealing, precision PCM charging |

Pulsating Heat Pipes (PHPs)
Pulsating Heat Pipes (PHPs), also called Oscillating Heat Pipes (OHPs), are passive two-phase heat transport devices that operate through self-excited oscillation of liquid slugs a
| Wick structure | None (wickless) |
| Minimum device thickness | < 3 mm |
| Maximum transport distance | > 1 m |
| Compatible working fluids | Ammonia, propylene, R245fa, acetone |

Space Copper-Water Heat Pipes (SCWHPs)
Flight-proven copper-water heat pipes for high heat flux satellite electronics cooling, capable of handling up to 50 W/cm² with first flight heritage from ISS in 2017.
| Heat flux capability | Up to 50 W/cm² |
| Temperature gradient (typical) | 2–5°C |
| Wicking capability against gravity | Up to 10 inches |
| Minimum bend radius | 3× OD |
| Generation | GEN III manufacturing process |

Space Liquid Cooling Systems
Custom single-phase liquid cooling loops for spacecraft applications, integrating cold plates, accumulators, cooling lines, and heat exchangers to manage high-heat-flux electronics
| Cooling type | Single-phase liquid (pumped fluid loop) |
| Components | Cold plates, accumulators, cooling lines, heat exchangers, liquid cooled chassis |
| Accumulator functions | Pressure control, volume compensation, transient dampening |

Thermo-Modulating Heat Pipes (TMHPs)
A dual-mode spacecraft thermal device combining VCHP and thermal diode functions in a single gas-charged aluminum-ammonia design, eliminating the separate NCG reservoir for reduced
| Working fluid / envelope | Aluminum-ammonia |
| Ncg reservoir | Integrated (no separate reservoir) |
| Demonstrated load (VCHP Mode) | ~36 W |
| Operating modes | VCHP mode (forward); Diode mode (reverse blocking) |
| Control method | Passive (Non-Condensable Gas) |

Vapor Chambers
Planar two-phase heat spreaders with effective thermal conductivities of 5,000–200,000 W/m·K, available in standard copper/water and advanced low-CTE aluminum nitride ceramic varia
| Standard planar dimensions | Up to 10" × 20" |
| Standard heat flux | > 100 W/cm² |
| Standard thermal resistance | < 0.08°C/W |
| Effective thermal conductivity range | 5,000–200,000 W/m·K |
| Low-cte variant max heat flux | > 700 W/cm² (1 cm² area) |

Variable Conductance Heat Pipes (VCHPs)
Passive spacecraft thermal control devices combining two-phase working fluid with a Non-Condensable Gas reservoir to automatically regulate evaporator temperature across wide power
| Effective thermal conductivity | 10,000 to 100,000 W/m·K |
| Control method | Passive (Non-Condensable Gas) |
| Material systems available | Aluminum-ammonia; Copper-monel/water; Sodium-Haynes |
| Quality certification | ISO 9001:2015, AS9100D |
Aerospace Fabrication and Materials, LLC
United States · 17 productsAerospace Fabrication and Materials, LLC designs, manufactures, and installs multilayer insulation (MLI) blankets and passive thermal control products. They also fabricate soft goods and insulation solutions for extreme aerospace and cryoge

AstraWrap™ HT
AstraWrap™ HT is a prefabricated multilayer insulation layup designed for high-temperature space applications up to 500°F, combining polyimide film with Dacron netting for optimal
| Standard material width | 48 inches |
| Standard length | 10 linear feet |
| Operating temperature | -452 (-269) to +300 (149) °F(°C) |

AstraWrap™ Thermal Insulation Space Wrap
AstraWrap™ is a versatile thermal insulation wrap, ideal for aerospace applications including satellites, launch vehicles, and space stations, ensuring optimal thermal performance
| Film Thickness | 0.25 mil (6 µm) |
| Max Temperature | 250°F |
| Standard Length | 10 feet |
| Standard Width | 48 inches |
| Custom Width | up to 54 inches |

Cryogenic Cabling
Cryogenic cable superinsulation is built from a combination of reflective thin films and low thermally conductive fabric spacer material that lessens heat flux, effectively maintai

Cryogenic Multilayer Superinsulation
Aerospace Fabrication offers quality cryogenic multilayer superinsulation systems for thermal control in various applications, including cryogenic cabling and tank insulation.
| Operating temperature | below -100 °C |

Cryogenic Tanks
Aerospace Fabrication & Materials produces a wide range of engineered solutions for cryogenic tanks, systems, and subsystems, providing effective thermal control in vacuum envi

Custom Soft Goods Manufacturing
Aerospace Fabrication & Materials offers custom fabricated covers for environmental protection of space-bound hardware, including passive thermal protection, impact resistance,

High Temperature Plume Shields
AFM fabricates specialized MLI blankets and plume shields designed to withstand extreme high temperatures around engine nozzles and other heat sources.
| Temperature Range | 300C to 1,000C and above |

MMOD Shields
AFM’s MMOD shields utilize cutting-edge materials, including Beta Cloth, Kevlar®, and Nextel® fabrics, to provide unparalleled protection for spacecraft against high-velocity micro

Multilayer Insulation Blankets
Multilayer Insulation (MLI) blankets provide passive thermal control to a variety of spacecraft, launch vehicles, and instruments in vacuum by limiting radiative heat transfer.
| Operating temperature | -250…+1300 °C |

PolaLam
PolaLam™ is a durable cryogenic insulation laminate designed for enhanced handling and increased tear resistance without significant thermal performance sacrifice.
| Spacer layer thickness | 5.0 mil |
| Roll Width | 2 inches |
| Roll Length | 100 linear feet |
| Operating temperature | -452 °F |
| Areal Density per layer pair | 0.034 kg/m2 |

PolaPair™
PolaPair™ is a cryogenic superinsulation subsystem combining a single reflector layer and separator, available in standard lengths and custom widths for various insulation system r
| Standard Lengths | 100, 200, and 500 feet |
| Custom Widths | up to 86 inches |
| Aluminum Coating (PP001-56) | One Sided |
| Crinkled (PP001-56) | No |
| Perforated (PP001-56) | No |

PolaTape™
PolaTape™ is an aluminized reflective tape optimized for use in the construction and installation of cryogenic insulation systems, offering excellent reflective properties and flex
| Material | Polyester-based aluminized reflective tape |
| Roll Length | 216 linear feet |
| Standard Widths | 1-inch, 2-inch |
| Minimum Order Quantity | 1 roll |

PolaWrap™
PolaWrap™ is a custom prefabricated layup of superinsulation, available in standard configurations of 10 feet length and custom widths up to 86 inches.
| Reflector separation spacer thickness | 5.0 mil (127 µm) |
| Standard material width | 56 inches |
| Standard length | 10 linear feet |
| Maximum width | 86 inches |
| Number of layers (standard options) | 10, 15, or 20 Layers |

Radiators
Aerospace Fabrication personnel can provide specialty coated tapes for use as First Optical Solar Reflectors (FOSR) and are experienced in their application and installation for sa

Spacecraft Components
Aerospace Fabrication's spacecraft components feature MLI blankets and associated passive thermal control systems, offering a range of solutions from satellite components to rocket

Specialty Materials
Aerospace Fabrication and Materials offers a variety of high-performance specialty materials designed for demanding aerospace and cryogenic thermal applications.
| PolaWrap Length | 10 feet |
| PolaWrap Width | 86 inches |
| PolaLam Length | 100 feet |
| AstraWrap Length | 10 feet |
| AstraWrap Width | 54 inches |

Sun Shields
Aerospace Fabrication & Materials offers custom Sun Shields designed to meet individual customer needs and requirements, with experience in designing and producing shields and
| Dimensions | up to 3 meters |
Airbus Defence and Space
France · 2014 · 1 productAirbus Defence and Space designs and manufactures satellites, spacecraft equipment, and provides related services for telecommunications, navigation, Earth observation, and space exploration.

High Performance Radiator technology (HiPeR) Flexlinks
HiPeR Flexlinks are highly flexible thermal straps developed by Airbus for spacecraft thermal control, offering superior conductance-to-mass ratio compared to traditional solutions
| Conductance-to-mass ratio | three to five times higher than traditional solutions (W/K per kg) |
| Lead time | about 4 months (average) |
| TRL | 9 |
| Flight heritage | on-board missions in Telecom, Science, Earth Observation and megaconstellations |
| Conductivity | up to 3.6 W/K |
Akash Systems
United States · 1 productUS developer of GaN-on-Diamond satellite radios and power amplifiers delivering 3-5x higher data rates through proprietary Diamond Cooling technology.

GPU on Diamond
Experience exponentially increased compute, lower failure rates, and less energy consumption with Diamond Cooling for GPUs.
Allatherm
Latvia · 3 productsLatvian company making heat pipes and loop heat pipes for space thermal management, collaborating with ESA, Airbus D&S, Thales, DLR, and JAXA, and developing a Xenon compressor for ESA Lunar Gateway.

Altom10 Series — LHP Evaporator Modules for Microelectronics
Modular Loop Heat Pipe evaporator modules for microelectronics thermal management — up to 10 m separation, several thousand times the thermal conductivity of copper.
| Materials | Copper (Cu) and Stainless Steel (SS) |
| Charge chamber volume | 1–7 cc |
| Footprint range | 28×50 mm to 100×50 mm |
| Max condenser separation | Up to 10 m |
| Effective thermal conductivity | Up to thousands times solid copper |

Altom14 Series — LHP Evaporator Modules for Power Electronics
High-performance stainless steel Loop Heat Pipe evaporator modules for power electronics cooling — ISO 3834-2 certified welding, manufactured in ISO 8 cleanroom.
| Material | Stainless Steel (SS) |
| Configuration options | 1-slot to 3-slot (1SL, 2SL, 3SL) and multi-channel variants |
| Representative sizes | 40×160 mm (1SL), 100×140 mm (2CPL) |
| Charge chamber volume | 2 cc (typical) |
| Manufacturing standard | ISO 3834-2 welding, ISO 8 cleanroom |

Gas Thermal Compressor
Passive, vibration-free thermal compressors for Xenon, Krypton, and Hydrogen gases reaching 200–400+ bar — no moving parts for space propulsion gas management.
| Gases handled | Krypton, Xenon, Hydrogen, hydrocarbons |
| Output pressure | 200–400+ bar |
| Vibration | Negligible (passive thermal operation) |
| Applications | Satellite propulsion gas management, space instruments, in-orbit refueling |
Arquimea
Spain · 2007 · 7 productsSpanish space technology company founded 2007 in Leganes, developing MEMS relay switches, SiC power devices, and miniaturized power conditioning units for satellite applications.

Deployable Radiators for Satellites
Foldable deployable thermal radiator panels based on multi-loop heat pipe architecture for telecommunications satellites, stowed for launch and deployed in orbit to reject high hea
| Architecture | Multi-Loop Heat Pipes (LHP) with embedded condenser lines |
| Maximum radiator surface | Up to 6 m² |
| Temperature operating range | -160°C to +120°C |
| Power range | 1 W to 1,000 W |
| Working fluids | Ammonia, propylene, ethane |

Heat Pipes for Space Applications (Axial, Arterial, Diode)
Space-qualified axial grooved, arterial, and diode heat pipes in aluminum or stainless steel for satellite thermal control, carrying 5–500 W over temperatures from -130°C to +145°C
| Heat pipe types | Axial grooved, arterial, diode |
| Materials | 6063 aluminum alloy (axial); stainless steel (arterial) |
| Working fluids | Ethane, propylene, ammonia, toluene |
| Temperature operating range | -130°C to +145°C |
| Power range | 5 W to 500 W |
IberEspacio Satellite Thermal Control Hardware
Flight-proven heat pipes, loop heat pipes (LHP), MLI blankets, and thermo-structural panels for satellite thermal management — >1,000 units delivered across 53+ missions includi
| Heat transfer capacity (LHP) | Up to 1 kW standard; >1.2 kW multi-evaporator |
| Operating temperature range (LHP) | 140 K to 400 K (−133°C to +127°C) |
| High-temperature lhp | Up to 125°C (HTLHP, TRL 5+) |
| Max lhp transport length | Up to 10 m |
| Working fluids | Ammonia, propylene, ethane, Freon R134a |

Loop Heat Pipes for Space Applications
Fully customized two-phase passive Loop Heat Pipes (LHP) for satellites, offering up to 1 kW heat transfer power, mechanical decoupling, and lifetime exceeding 15 years, with 52 un
| Heat transfer power | Up to 1 kW |
| Temperature operating range | 140 K to 400 K (-133°C to +127°C) |
| Capillary pressure (ammonia) | 4 × 10⁴ Pa |
| Thermal resistance | From 0.005 °C/W |
| Transport line length | >5 m |

Thermal and Structural Subassemblies for Space
Turnkey integrated thermal and structural subassemblies for thermally demanding satellite systems including active antenna arrays, cryogenic sensors, optical laser terminals, and p
| Subsystem types | Laser terminal thermal systems, spacecraft modular thermal platforms, LNA thermal systems, |
| Temperature range coverage | Cryogenic (down to 20 K) to high temperature (up to +450°C) |
| Engineering scope | Design, thermal/mechanical analysis, simulation, manufacture, integration, test |
| Units in orbit | 10 |
| Units awaiting launch | 18 |

Thermal Blankets for Space Applications (MLI)
Custom multi-layer insulation (MLI) thermal blankets for spacecraft, covering internal and external applications from cryogenic temperatures down to 20 K through high-temperature e
| Mli types | Standard plastic MLI, sewn fabric coated MLI, external MLI, internal MLI, SLI, high-temper |
| Temperature range — typical | -150°C to +150°C |
| Temperature range — cryogenic | Down to 20 K |
| Temperature range — high temperature | Up to +450°C |
| Materials | Kapton®, Upilex®, Mylar®, FEP (Teflon)®, Dacron®, Beta Cloth®, Nextel®, glass fiber, Velcr |

Thermo-Structural Radiator Panels for Space
Aluminum honeycomb thermo-structural radiator panels serving as satellite structure while dissipating heat, with optional embedded heat pipe networks up to 6 kW per panel, delivere
| Panel materials | Aluminum skins + aluminum honeycomb core |
| Maximum panel size | Up to 18 m² |
| Power dissipation (with embedded heat pipes) | Up to 6 kW per panel |
| Operating temperature | -40°C to +130°C |
| Heat pipe integration | Available with or without embedded heat pipes; mono-level to multi-level networks |
Boyd Corporation
United States · 2 productsUS manufacturer of engineered material solutions — sealing, EMI shielding, thermal management, and protection technologies — for aerospace, defense, and other demanding industries.

k-Core Encapsulated Graphite Thermal Solutions
Boyd Corporation's k-Core is a proprietary encapsulated Annealed Pyrolytic Graphite thermal-conduction material used to build lightweight, high-conductivity radiator panels, therma
| Effective thermal conductivity (k-Core assembly) | up to 1000 W/m·K |
| Apg core in-plane thermal conductivity | up to 1700 W/m·K |
| Thermal straps effective conductivity | up to 1200 W/m·K |
| Radiator panel operating temperature range | -40°C to +72°C |
| Heat dissipation improvement | ≥40°C reduction vs. aluminum equivalent |

Spacecraft Thermal Management Systems
Boyd Corporation's (Aavid) space-grade thermal management solutions — heat pipes, vapor chambers, thermal straps, and two-phase cooling systems for satellite electronics.
| Products | Heat pipes (CCHP/VCHP), vapor chambers, thermal straps, thermal interface materials |
| Heat pipe working fluids | Ammonia (space standard), water, ethanol |
| Thermal straps | Braided copper or graphite fiber; flexible isolation |
| Thermal interface | Indium foil, phase-change materials, filled epoxies |
| Standards | Space-qualified assemblies (ASTM/AIAA); MIL-SPEC screened materials |
Calyos
Belgium · 4 productsBelgian expert in passive two-phase cooling technologies — heat pipes, loop heat pipes, and pulsating heat pipes — for thermal management in aerospace, defense, and industrial applications.

Heat Pipes (HP)
Traditional heat pipe technology providing low thermal resistance passive cooling — scalable to application size, exploits latent heat of vaporization.
| Technology | Latent heat of vaporization, wick return |
| Applications | Data centers, embedded electronics, batteries, power electronics |

Loop Heat Pipes (LHP)
Long-distance passive heat transport for high heat flux applications — up to 100% less power, 10x lifetime, and 30% less weight than water-based cooling.
| Power vs. water-based cooling | Up to 100% less |
| Lifetime vs. water-based cooling | Up to 10x |
| Weight vs. water-based cooling | Up to 30% less |

Micro Channel Heat Pipes (MCHP)
Hybrid HP-PHP flat aluminium heat pipe design — lightweight, customizable in length and bends, for batteries and embedded electronics.
| Design | Flat aluminium, customizable length and bends |
| Applications | Batteries, embedded electronics, radar/lidar sensors |

Pulsating Heat Pipes (PHP)
Oscillating heat pipe technology with less reliance on gravity — customizable thin/3D form factors, PHP Spreader research prototype dissipates 800W.
| Php spreader dissipation | 800 W |
| Applications | Power electronics, inverters, on-board chargers, sensors |
CAVU Aerospace
United Kingdom · 2016 · 1 productCAVU Aerospace designs and manufactures spacecraft avionics, including radiation-tolerant onboard computers, thermal control units, frame grabbers, and flight-proven satellite cameras for space applications.

Thermal Control Unit
Smart efficient thermal management for space systems
| Dimensions (L×W×H) | 160 mm × 170 mm × 38 mm |
| Mass | 1,000 gr (Std. version) |
| Power consumption | 1.5 W ~ 3 W |
| Supply voltage | 28 V / 75 V ±4 V |
| Interfaces | CAN, RS422 RS485, RS232, GPIO, Debug: JTAG, SoftConsole or Keil |
DHV Technology
Spain · 2013 · 2 productsDHV Technology is a Spanish space technology company designing and manufacturing solar panels, electrical power systems, MLI blankets, and solar array drive assemblies for CubeSats and small satellites. Based in Málaga since 2013.

MLI Blankets
Custom multi-layer insulation (MLI) blankets for CubeSats and small satellites, providing passive thermal control to maintain temperature within operational limits.

Multi-layer Insulation Blankets
Multi-Layer Insulation blankets are thermal insulators conformed by multiple layers of optical and electrically conductive materials separated by thin netting spacers.
DUNMORE
United States · 1970 · 5 productsUS manufacturer of coated and metallised films (Bristol, PA); MLI thermal blankets and spacecraft thermal management films for satellite and space applications; 50+ years experience.

Aerospace Tape (Spacecraft Thermal Control Tape)
Thermal control tape line for spacecraft — MLI blanket tape, aluminized/black Kapton tapes, radiator tapes, using flight-proven non-silicone adhesives.
| Variants | Second Surface Aluminized Kapton Tape, Stamet Coated Black Kapton Tape, Germanium Coated B |
| Adhesive types | Conductive and non-conductive PSA |

DUN-COOL Thermal Management Film
Passive thermal control film functioning as a spacecraft radiator or optical solar reflector — low solar absorptance, high emittance, ATOX resistant.
| Function | Radiator or optical solar reflector (OSR) |
| Purpose | Passive thermal management, radiation protection, heat rejection |

DUN-DIFFUSE White Kapton Polyimide Film
White Kapton polyimide film offering high emissivity thermal control — alternative to paint for spacecraft MLI outer layer or radiator second-surface mirror.
| Base film | 100 Ga (25 micron) |
| Metalization | Vacuum Deposit Aluminum (VDA) |
| Coating options | ITO or StaMet |
| Variants | ITO/100Ga White Kapton WS/VDA, StaMet/100Ga White Kapton WS/VDA |

Multi-Layer Insulation
Multi-Layer Insulation films from DUNMORE Aerospace are used to manufacture MLI blankets for passive thermal control systems in space.

Satkit MLI Satellite Kit
Pre-cut multi-layer insulation kit with STARcrest MLI materials sized for small satellite developers to build custom thermal protection blankets.
| Kit contents | Outer layer material roll, inner layer material roll, polyimide assembly/edge-binding tape |
| Target platforms | CubeSat form factors (1U-6U) |
Glavkosmos
Russia · 1985 · 12 productsGlavkosmos coordinates international human spaceflight projects, facilitates satellite launches, develops and supplies rocket components, and provides equipment for space crews.

Absolute Pressure Sensor Vt 220
The Absolute Pressure Sensor Vt 220 is a flight-qualified strain gauge sensor designed to measure absolute pressure of liquid and gaseous media in satellite telecontrol and thermal
| Range of measurements | 0-0.125; 0-0.250; 0-0.500 |
| The basic error | ±1 % |
| The normalizing value of the output signal, mv / v | 2.25±0.8 |
| Supply voltage | 6+0.3-1.2 |
| Mass | 0.16 kg |

Arterial Heat Pipes
Arterial Heat Pipes (AHPs) are two-phase, hermetic closed thermal transfer systems designed for spacecraft thermal control, offering high heat transfer capabilities and a long serv
| Purpose | Thermal control of spacecraft equipment. |
| Year of release | 1992 |
| Design life | 25 years after ArHP filling with working fluid. |
| Lead time | 3 months |
| Flight qualification of the product | Yes |

Axial Grooved Heat Pipes
Flight-proven spacecraft heat pipes (450 W·m transfer, Ø6–20 mm, up to 6 m, -133 to +227 °C) with 100+ satellite heritage. Customizable.
| Purpose | Thermal control of spacecraft equipment |
| Year of release | 1996 |
| Design life | 25 (after filling with working fluid) years |
| Lead time | 2 months |
| Flight heritage | Successfully operated on more than 100 Russian and foreign satellites |

Axial, Arterial, Contour Heat Pipes, Radiator Heat Pipe
This product line includes axial, arterial, and contour heat pipes and radiator heat pipes designed for thermal control in space applications.
| Purpose | Design and manufacture of products for providing thermal regime with flight application. |
| Flight qualification of the product | Yes |
| Brief history of flight qualification | Vast experience in all types of heat pipes and systems. |
| Possibility to adapt the product to customer requirements | Yes |
| Testing standard | European standard PSS49 |

Contour Heat Pipes
Contour Heat Pipes (CHPs) are two-phase thermal transfer systems designed for the thermal control of spacecraft equipment, offering flexible integration and high heat transfer capa
| Purpose | Thermal control of spacecraft equipment. |
| Year of release | 1992 |
| Design life | 25 years after CHP filling with working fluid. |
| Lead time | 6 months |
| Flight qualification of the product | Yes |

Electric Heaters
These Electric Heaters (EH) are flexible single-sided printed circuit boards designed to provide thermal conditions for spacecraft onboard equipment. They feature a resistive print
| Purpose | Designed to provide thermal conditions for spacecraft onboard equipment. |
| Year of release | 1976 |
| Design life | 36 years |
| Lead time | 3 months |
| Flight qualification of the product | Yes |

Electric Heaters for Manned Spacecraft
These electric heaters are flexible, single-sided printed circuit boards designed to maintain the surface temperature of manned spacecraft bodies and their fastening elements withi
| Year of release | 2015 |
| Design life | 15 years |
| Lead time | 4 months |
| Flight qualification of the product | No |
| Possibility to adapt the product to customer requirements | Yes |

Low Temperature Heat Pipes
Low Temperature Heat Pipes are designed to ensure the thermal regime of spacecraft, utilizing ammonia as a heat carrier and featuring axial omega-shaped grooves.
| Purpose | Aggregate of systems for ensuring the thermal regime of the spacecraft. |
| Year of release | 1973 |
| Design life | 23 years |
| Lead time | 3 months |
| Flight qualification of the product | Yes |

Radiation Refrigerator
A passive radiation refrigerator designed to cool radiation receivers to cryogenic temperatures in space, with flight heritage on Meteor-M and Electro-L satellites.
| Year of release | 2003 |
| Design life | 10 years |
| Lead time | 6 months |
| Flight qualification of the product | es |
| Brief history of flight qualification | KA Meteor-M, Electro-L. |

Screen-Vacuum Thermal Insulation of Orbital Spacecraft
Screen-Vacuum Thermal Insulation (SVTI) is a passive thermal control system for orbital spacecraft, designed to reduce heat transfer and protect against micrometeorites and space d
| Flight qualification of the product | Yes |
| Brief history of flight qualification | Vast work experience. |
| Possibility to adapt the product to customer requirements | Yes |

Temperature-controlled Honeycomb Panel
Temperature-controlled honeycomb panels designed for spacecraft platforms and payload equipment, featuring aluminum face sheets and options for integrated heat transfer tubes or fl
| Flight qualification of the product | Yes |
| Brief history of flight qualification | Flight qualification since 2000. |
| Possibility to adapt the product to customer requirements | Yes |
| Maximum dimensions | 5800 × 3000 mm |
| Honeycomb filler | Amg5-N-6-23P/Amg5-N-2.5-23P/Amg2-N-2.5-40P/Amg2-N-2.25-50P (rus) |

Thermal-Protection Materials for Spacecraft
Nonablative thermal-protection silica-fiber-reinforced materials for coating reusable spacecraft and for radio engineering-purpose articles.
| Purpose | Provision of normal thermal conditions on passing the dense atmosphere at landing, antenna |
| Year of release | 1977 |
| Lead time | Depending on the volume of an order |
| Flight qualification of the product | Yes |
| Brief history of flight qualification | Spacecraft Buran. |
Hemeria
France · 1 productHEMERIA designs, produces, and supplies space systems, vehicles, and defense equipment for commercial, institutional, and scientific customers.

MLI
HEMERIA designs, builds, tests and integrates thermal control subsystems used in all types of applications (commercial, defense, scientific).
Lidax
Spain · 2 productsMadrid-based aerospace engineering company specialising in opto-mechanical systems, flexible thermal straps, and cryogenic units for space missions.

Flexible Thermal Straps
LIDAX Flexible Thermal Straps (FTS) are high-performance solutions for efficient and reliable heat transfer in space applications, available in copper and pyrolytic graphite.
| Materials | High Thermal Conductivity Materials (Copper, Pyrolytic Graphite) |
| Copper fts applications | Electronic units and power systems, High-stability payloads, Cryogenic applications, Platf |
| Pyrolytic graphite fts applications | New Space platforms, payloads and high-sensitivity instrumentation |
| Offerings | Qualified Standard Solutions, Mission-Specific Customization |
| Interface material | OFHC Copper |

PSG Thermal Links (Pyrolytic Graphite Flexible Thermal Straps)
LIDAX’s PSG Thermal Links are flexible thermal straps manufactured from pyrolytic graphite sheet (PGS), engineered for space missions where high thermal conductance combined
| Material | Pyrolytic Graphite Sheet (PGS) |
| Type | Flexible Thermal Strap (FTS) |
| Applications | Focal plane assemblies, cryo-cooler interfaces, deployable radiators |
| Mission heritage | BepiColombo, EarthCARE, PLATO, James Webb Space Telescope |
MAP (Aerospace Coatings)
2 productsMAP is a European aerospace surface treatment and coatings company specializing in thermal control coatings, optical solar reflectors, and surface preparation materials for spacecraft and satellite applications. The company's products inclu

MAP SPACE COATINGS (Company Profile)
MAP SPACE COATINGS specializes in the design, manufacture, and application of thermal finishing coatings for satellites and launchers, emphasizing a zero-defect policy and technolo
| Color | White |
| Formulation | Water-based polyurethane |
| Properties | Antistatic, low outgassing, thermo-optical control |
| Compliance | REACH |

MAP SPACE COATINGS Thermal Finishing Services
MAP SPACE COATINGS provides specialized thermal finishing services for satellites and launchers, encompassing the design, manufacture, and application of thermal coatings.
| Coating type | Water-based, silver-loaded polyurethane |
| Function | EMI shielding, electrical continuity |
| Application | Launcher fairings |
Minco Products, Inc
United States · 15 productsMinco Products, Inc. designs and manufactures solutions for heating, flex circuits, temperature sensing, and instrumentation. They offer off-the-shelf products and craft customized solutions in partnership with engineering teams.

All-Polyimide (KAPTON®) Heaters
Minco's all-polyimide heaters offer a high-performance alternative to standard polyimide flexible heaters, supporting higher temperatures and greater watt densities for demanding a
| Maximum operating temperature | 260°C |
| Max. size | 560 mm x 1145 mm |
| Max. resistance density | 230 Ω/in² |
| Temperature range | -200 to 200 °C |

Controllers
Minco specializes in standard and fully integrated custom control applications that leverage a variety of control methods, with versatile packaging options to meet various size, sh
| Operating temperature | -50 to 260 °C |
| Pressure rating | 7000 psi |
| Insulation resistance | 10 megohms min. at 100 VDC |
| Temperature range | -50…+550 °C |
| Dimensions | 11.0" (279 mm) MAX extension |

Elements
Wire-wound and thin-film ceramic RTD elements deliver accurate, reliable and repeatable temperature measurement over a wide temperature range.
| Temperature range | -50 to 260 °C |
| Pressure rating | 3.4 bar |

Humidity Sensors
Minco humidity sensors deliver reliable, accurate readings across a variety of applications, including those in aerospace and defense.
| Operating temperature | -50 to 260°C |
| Pressure rating | 7000 psi (483 bar) at 21°C |
| Insulation resistance | 10 megohms min. at 100 VDC |
| Time constant (Grounded junction) | 17 seconds |
| Time constant (Ungrounded junction) | 22 seconds |

Mica THERMOFOIL TM Heaters
Mica Thermofoil heaters deliver flexible wattage capacity capable of providing uniform heating across a variety of shapes and sizes, ideal for applications requiring fast warmup an
| Watt Density | up to 110 W/in² |
| Temperature Range | -150°C to 600°C (-238°F to 1112°F) |
| Max. size | 560 mm x 1168 mm |
| Max. resistance density | 3.9 Ω/cm² |

Miniature Sensors
Minco's miniature temperature sensors are small-profile sensors that save space and weight while providing fast thermal response time and designs suitable for high levels of vibrat
| Temperature range | -50 to 260 °C |
| Pressure rating | 50 psi |

Polyimide (Kapton®) Thermofoil™ Heaters
Flexible polyimide Thermofoil™ heaters offer rugged, reliable performance in a thin, lightweight package, ideal for maximizing thermal transfer when space and weight are limited.
| Mass | 0.009 oz/in² |
| Dimensions | 0.010” (0.25 mm) thick over the element |

Probes & Probe Assemblies
Minco's advanced temperature probe sensor technology comes in multiple standard and custom-engineered configurations to meet diverse requirements for aerospace and other demanding
| Temperature range | -50 to 260 °C |
| Pressure rating | 3.4 bar |

PTFE (Teflon) Heaters
Minco's PTFE (Teflon) heaters provide clean, non-stick thermal transfer designed to withstand tough applications, including those in aerospace and medical equipment.
| Operating temperature | -200 to 150°C |
| Maximum size | 10"×40" |
| Heater thickness Over element | 0.060" |
| Heater thickness Over leadwire terminations | 0.150" |
| Dielectric strength | 1000 VRMS at 60 Hz for 1 minute |
Silicone Rubber Heaters
Minco's flexible silicone rubber heaters are designed for large-size, industrial applications requiring precise, reliable thermal transfer and excellent abrasion resistance in rugg
| Operating temperature | -45 to 235 °C |
| Max. size | 560 mm x 2285 mm |
| Max. resistance density | 31 Ω/cm² |
| Insulation | Silicone Rubber |

SmartHeat™ SLT Thin-Film Heaters
SmartHeat SLT uses a patented polymer compound to produce a thin film heater that controls temperature without the need for external sensors or controllers, ideal for critical temp
| Temperature range | -45°C (-49°F) to 100°C (212°F) |
| Set point range | 10°C (50°F) to 70°C (158°F) |

Stator Sensors
Flat, laminated stator RTDs from Minco deliver accurate temperature measurement between stator windings to prevent motor overheating in demanding applications.
| Operating temperature | -50 to 260°C (-58 to 500°F) |
| Pressure rating | 7000 psi (483 bar) at 21°C, reducing to 6300 psi (433 bar) at 260°C |
| Insulation resistance | 10 megohms min. at 100 VDC |
| Time constant | 17 seconds (Grounded junction), 22 seconds (Ungrounded junction) |

Surface Sensors
Minco’s Thermal-Ribbon™ sensors are thin, flexible RTDs and thermocouples designed for surface or pressure sensitive adhesive mounting, offering non-invasive and rapid tracking of
| Temperature range | -50 to 260 °C |
| Pressure rating | 3.4 bar |

Temperature Sensors
Minco offers a wide range of standard and custom-engineered temperature sensors for reliable, accurate, and cost-effective temperature measurement across various specialized uses,
| Thermocouples Temperature Range | -200°C to 2300°C |
| RTDs Temperature Range | -200°C to 850°C (industrial grade Pt), up to 962°C (laboratory grade Pt) |
| Thermistors Temperature Range | -80°C to 300°C |
| Thermocouples Accuracy | Fair |
| RTDs Accuracy | Good |

Thermal-Clear TM Transparent Heaters
Thermal-Clear heaters provide an accurate, reliable heat source without blocking light, ideal for high visibility use cases in aerospace and other demanding applications.
Northrop Grumman Space Systems
United States · 1939 · 1 productMinotaur family, Pegasus XL, Antares (legacy); MLV co-development with Firefly.

Cryocoolers
Northrop Grumman's pulse tube cryocoolers provide high reliability for critical space missions, operating without moving parts for extended lifespans.
| On-orbit operation | More than 300 combined years |
| Operating mechanism | Without moving parts |
| Applications | Missile defense, climate science, astronomy, weather tracking and prediction |
| Scalability | Scalable for large-scale and robust spacecraft, and for smaller, more proliferated spacecr |
| Flight heritage | NASA’s James Webb Space Telescope |
Paragon Space Development Corporation
United States · 1993 · 1 productUS life support and thermal control engineering company providing environmental control systems, spacesuits, and thermal management solutions for NASA, commercial, and defense space programs.

xRAD™ Extruded Thermal Control Radiator
Patented extruded aluminum thermal control radiator for spacecraft and launch vehicles, eliminating inefficiencies of traditional bonded radiator structures.
| Technology | Extruded aluminum panels with integral coolant channels (patented) |
| Function | Active thermal control — heat rejection to space |
| Applications | Spacecraft radiators, satellite thermal control, launch vehicle cryogenic insulation |
| Flight heritage | Sierra Space Dream Chaser Cargo Module |
| Product variants | SatRad (satellite), high-turndown radiators, high-energy storage thermal management |
Peraton Space
United States · 1 productUS national security technology company providing satellite communications, space domain awareness, ground systems operations, and intelligence support services to the US government and military.

Acusil® Thermal Protection System (TPS)
Acusil® is a lightweight, silicone syntactic foam-based thermal protection system designed to shield high-value assets like spacecraft and strategic weapons systems from intense he
| Acusil® ii ablation resistance | zero ablation in heat fluxes up to 100 W/cm2 |
| Acusil® iv ablation resistance | withstands up to 150 W/cm2 |
| Durability | Decades (30+ years) |
Pumpkin, Inc.
United States · 1995 · 1 productSan Francisco-based manufacturer of flight-proven CubeSat kits, SUPERNOVA nanosatellite buses, and spacecraft power/electronics components, with over 150 kits delivered and dozens of successful space missions since 2003.

SR630 Thermocouple Monitor Replacement Thermal Shield
Replacement thermal shield for Stanford Research Systems (SRS) SR630 16 Channel Thermocouple Monitor and rebranded units of the same design.
RUAG Space
Switzerland · 1993 · 4 productsSwiss-Swedish space components manufacturer providing satellite structures, thermal control products, payload electronics, and antennas for commercial and institutional programs.

Conductive Glass Fabric High-Temperature Vacuum Insulation
Flexible high-temperature vacuum insulation for launchers up to 550 degrees C, free of hazardous components and tunable to customer requirements.
| Maximum temperature | Up to 550 degrees C |
| Type | High temperature vacuum insulation, conductive glass fabric |
| Advantages over ceramic fabrics | Greater flexibility, no hazardous components, adjustable performance |
| Weight | 429 g/m2 ±5% |
| Thickness | 0.4 mm ± 5% |

COOLCAT Cryogenic Superinsulation
Multi-layer vacuum superinsulation line for cryogenic applications, laser-cut to shape, with polyester, aluminium-foil, LOX-compatible and tape variants.
| Coolcat 2 nw | 10 layers double-sided aluminized perforated polyester foil interleaved with 10 layers of |
| Coolcat 2 nf | Glass fibre fleece spacer with 9 micrometre pure aluminium foil; high temperature tolerant |
| Coolcat 2 lox | 5 layers pure aluminium foil with 5 layers glass fibre cloth spacer; liquid oxygen compati |
| Coolcat 2 ni | Polyester foil aluminized in squares (10x10 mm single-sided or 20x20 mm double-sided) with |
| Coolcat h | Welding protection of aluminium foil and fibre-glass cloth |

Flexible Thermal Protection for Launchers
Coated or laminated ceramic fabric and ceramic felt insulation protecting components near rocket motors and nozzles at up to 1500 degrees C.
| Maximum temperature | Up to 1500 degrees C |
| Materials | Coated or laminated ceramic fabric and ceramic felt insulators |
| Application | Components in direct vicinity of rocket motors or nozzles |
| Density (Ceramic Felt for 1500°C) | 100 – 130 kg/m3 |
| Mass (Ceramic Felt for 1500°C, 13mm thickness) | 1270 – 1650 g/m2 |

Satellite Multi-Layer Insulation (MLI)
Custom satellite MLI blankets for 1 K to 1800 K, with MMOD and ATOX protection options, produced for over 800 satellites.
| Operating temperature | 1 K to 1800 K |
| Protection options | MMOD (micrometeoroid orbital debris) and ATOX (atomic oxygen) |
| Design process | Electronic 3D models; 3D mock-ups and template fit-checks for complex shapes |
| Related products | Interfillers, sensors and heaters, thermal analysis and correlation services |
| Flight heritage | MLI for over 800 satellites across 50 space projects; Euclid, Juice, BepiColombo, Eutelsat |
Sheldahl (Multek Flexible Circuits)
United States · 1959 · 1 productSheldahl (Multek Flexible Circuits) is a US manufacturer of flexible printed circuits, printed electronics, electronic materials, and aerospace thermal control materials, headquartered in Northfield, Minnesota.

Aerospace Thermal Control Materials
Flight-proven thin-film thermal control materials protecting spacecraft since 1958, including JWST sunshield materials.
| Flight heritage | Space thermal control material heritage since 1958 |
| Notable program | James Webb Space Telescope onboard thermal protection |
| Material types | Multi-layer insulation, second-surface mirrors, conductive/non-conductive tapes, thermal c |
| Manufacturing processes | Vacuum deposition, adhesive formulation and laminating, slitting and sheeting |
| Application | Spacecraft and satellite thermal management in vacuum/radiation environments |
SPUTNIX
Russia · 2011 · 2 productsSPUTNIX is a Russian manufacturer of nanosatellite and microsatellite platforms, onboard subsystems and ground infrastructure, operating as a subsidiary brand of Sitronics Group.

Control unit of the thermal regime support system
A redundant thermal control unit (SX-SBOX-THERMU-01) that monitors and manages heaters based on analog/digital temperature sensors across the service platform and payload.
| Dimensions | 200 x 130 x 30 mm |
| Mass | 600 g |
| Supply voltage | 22-33 V |
| Power consumption without heaters included, no more | 5 W |
| Duplicated interface | CAN2B |

SX-SBOX Thermal Control (Microsatellite)
Thermal-control line of the SX-SBOX suite for microsatellite platforms: the thermal-control-system control unit (BU-SOTR) and engineering services for topology optimization.
| Thermal control unit sx-sbox-thermu-01 | 200 × 130 × 30 mm, 600 g, ≤5 W (heaters off) |
| Redundancy | 2 half-sets |
| Heater channels | 14 per half-set, ≤60 W each |
| Temperature sensors | 36 analog (P1K0) + 14 digital (DS18B20Z) per half-set |
| Topology optimization | SX-TOPOLOGY (engineering service) |
Technology Applications Inc (TAI)
United States · 1994 · 5 productsAmerican thermal strap manufacturer founded 1994 in Boulder CO; world's largest maker of flexible thermal links (copper, graphite, PGS); flown on Orion, OSIRIS-REx, Solar Orbiter, and Starliner.

Copper Cable Thermal Straps (CuTS)
OFHC copper-cable flexible thermal links used to passively conduct heat between spacecraft and cryogenic components, offered in 127 standard models plus fully custom designs.
| Material | 99.99 - 99.998% pure OFHC copper (Cu-101) |
| Cabling | TAI exclusive OFHC UltraFlex I (0.10 in / 2.5 mm) and UltraFlex II (0.20 in / 5 mm) copper |
| Standard models | 127 standard models, plus Cryocooler Series (72 sub-models) |
| Thermal conductivity | 397 - 2,500 W/(m-K) depending on temperature (4K - 300K) |
| Residual resistivity ratio (RRR) | 30 - 100 (typical 50-75, measured by Fermi, Argonne, and Brookhaven National Labs) |

Cryocooler Series Thermal Straps (CS-CuTS)
Standard copper thermal strap line sized to common Sumitomo (SHI) and Cryomech cryocooler cold-tip diameters, with 72 sub-models and free bolt-pattern/length customization.
| Material | 99.99 - 99.998% pure OFHC copper (Cu-101) |
| Cabling | TAI exclusive OFHC UltraFlex I (2.5 mm) copper cabling |
| Cold head diameters | 9 (2nd stage) cold head diameters available |
| Sub-models | 72 sub-models to choose from |
| Assembly method | Solder-free, never brazed or welded |

Graphite Fiber Thermal Straps (GFTS)
TAI provides the world’s only Graphite Fiber Thermal Links/Straps (GFTS), and the only carbon-based standard strap product line. GFTS assemblies are the space industry’
| Fiber material | GraFlex I / II carbon-fiber bundles; GraFlex III woven graphite fiber sheet |
| Fiber thermal conductivity | 800 - 1,000 W/(m-K) (GraFlex III); 2.75x copper's conductivity at room temperature |
| Density vs. copper | 1/4 the density of copper; 12x more thermal-conductivity/mass efficient than copper, 6x mo |
| Fabrication efficiency | Realizes up to 95% of material thermal conductivity |
| Mass | Most custom/standard straps weigh 10 - 30 g (1/5 - 1/10 the mass of an equivalent metallic |

PyroFlex PGS & Graphene Thermal Straps (X-Series)
TAI’s PyroFlex PGS (Pyrolytic Graphite Sheet) product line, also known as the X-Series, is the world’s highest thermal-performance, “ultra-low stiffness” th
| Material | Pyrolytic Graphite Film/Sheet (PGF/PGS), optional Graphene Layered Foil |
| Thermal conductivity | 1,350 - 2,500 W/(m-K), depending on material, temperature, and sheet thickness |
| Performance vs. metals | 6x the performance of aluminum and 4x the performance of copper at room temperature |
| Mass vs. metals | 28% lighter than aluminum; 77% lighter than copper |
| Stiffness | mN/mm range on all 3 axes when installed in curved/S-configurations (many measurements <=3 |

Thermally Conductive Vibration Isolation System (TCVIS)
Combined thermal-transport and 6-axis vibration-cancellation assembly for cryocooler-to-detector-dewar interfaces, co-developed with CSA Engineering and tested at NIST.
| Function | Combined thermal transport (via GFTS graphite fiber strap) and 6-axis active vibration can |
| Vibration reduction (axial, drive frequency) | > 40 dB (100:1 reduction) |
| Vibration reduction (radial, drive frequency) | 31 - 37 dB (37:1 to 70:1 reduction) |
| Harmonic reduction (next 4 harmonics) | Average 22 dB reduction |
| Isolation components | Compact electromagnetic actuators, force sensors, passive isolators |
Thales Cryogenics
Netherlands · 2000 · 3 productsDutch space cryocooler manufacturer in Eindhoven (Thales Nederland); Stirling, pulse tube, and J-T coolers for IR detectors at 10-200K; heritage on XMM-Newton, Herschel, Gaia, INTEGRAL.

LPT 9310 HP COTS+
The LPT 9310 HP COTS+ from Thales Group is a Pulse-Tube Cryocooler designed for space applications, offering a cooling capacity of 5.7 W.
| Cooling capacity | 5.7 W |
| Maximum input | 180 W |
| Mass | less than 7 kg |
| Dimensions | 24 x 90 x 204 mm |

LPT 9510 COTS+
The LPT 9510 COTS+ is a Split Pulse-Tube Cryocooler designed for space and scientific applications, offering 1.4 W cooling capacity at 80 K with low vibration and long lifetime.
| Cooling capacity | 1.4 W at 80 K |
| Maximum power input | 85 W |
| Mass | under 3 Kg |
| Dimensions | 18 x 122 x Ø 60 mm |

LPT6510 Pulse-tube Cryocooler
Designed-for-manufacturability pulse-tube cryocooler for 60 K and above, based on the flight-proven MPTC compressor.
| Max input | 60 W (AC); higher-power versions on request |
| Induced vibration | <2 N RMS in-axis |
| Operating temperature | -30 to +50 C (excl. qualification margin) |
| Off-state parasitic loss | Typical 0.45 W between 80 K and room temperature |
| Mass | < 3.2 kg |
Thermal Space Ltd.
United States · 4 productsUS thermal-management engineering firm in Boulder, Colorado, designing and manufacturing spacecraft thermal straps, cold plates, and cryogenic cooling hardware.

4C-PURE™ Cabled Copper Thermal Straps
Solderless, flexible copper thermal straps fabricated from 100% oxygen-free high-conductivity (OFHC) copper cable or braid, used to provide high thermal conductance with mechanical
| Material | OFHC Copper (C101, C10100), 99.99% purity |
| Residual resistivity ratio (RRR) | Typically 100–200 |
| Terminal hole diameter/location tolerance | 0.001-inch or better |
| Metallization options | Gold (Au), Silver (Ag), Nickel (Ni), Tin (Sn) |
| Product lines | 4C-PURE™ (standard), 4C-PURE-CRYO™ (low-temperature service with material certification an |

Custom Cold Plates
Custom-designed and fabricated cold plates (thermal control/interface plates) for heat sinking at a specified temperature, built from copper, aluminum, AlSiC, or graphite.
| Materials | Copper, aluminum, AlSiC, graphite |
| Cooling/heating methods | Refrigerant loops (HCFC/HFC/HC), cryogenic liquids (LN2, liquid methane), cryocoolers, the |
| Control inputs | Thermocouple, RTD, or thermistor |
| Communications | Serial, USB, or Ethernet |
| Control method | PID controller, push/pull heating/cooling |

Thermal LyNX®
A solid-state graphene thermal strap technology offering superior thermal conductance-to-mass ratio, high flexibility, and NASA-approved low-outgassing materials for spacecraft the
| Thermal conductivity-to-mass ratio | ~2x better than other thermal strap types |
| Thermal conductivity vs. aluminum (at ~220 K) | 16x per unit mass |
| Thermal conductivity vs. copper (at ~220 K) | 27x per unit mass |
| Elastic modulus vs. graphite fiber | ~20x lower (much more flexible) |
| Thermal conductivity-to-density ratio | >2x graphite fiber |

Thin Metal Foil Thermal Straps (TMF Series™)
The TMF Series™ Thin Metal Foil Thermal Straps, including Copper Foil Straps (CuFS™) and Aluminum Foil Straps (AlFS™), offer superior thermal and mechanical performance for various
| Copper type/purity | Electrical Tough Pitch (ETP), C110/99.9% |
| Rrr range | 50-100 |
| Copper type/purity (2) | Oxygen Free High Conductivity (OFHC), C101/99.99% |
| Rrr range (2) | 100-500 |
| Copper type/purity (3) | 4N/99.99% |
Thermavant
United States · 2007 · 1 productUS oscillating heat pipe (OHP) thermal management company; heat frames, chassis, radiators, and cold plates for space, airborne, and high-temperature electronics applications.

OHP Radiators
Oscillating heat pipe (OHP) embedded spacecraft radiators and structural panels for on-orbit waste-heat rejection, delivering up to 9x higher thermal conductance and 40% lower dens
| Simple radiator example thermal performance (OHP) | 2 °C rise per 150 W |
| Simple radiator example thermal performance (solid Al) | 18 °C rise per 150 W (9x worse than OHP) |
| Simple radiator effective density (OHP) | 1.6 g/cm³ (Al 6061 T4 w/ selective coating) |
| Simple radiator effective density (solid Al) | 2.7 g/cm³ (1.7x worse than OHP) |
| Simple radiator shape & size | Al 6061 T4, approx. 19" x 19" x 0.04-0.16" thick (variable thickness) |
Directory
Manufacturers in this sector
ACT (Advanced Cooling Technologies)
Premier thermal management solutions company specializing in custom two-phase heat transfer technology for aerospace, defense, and industrial applications.
Aerospace Fabrication and Materials, LLC
Aerospace Fabrication and Materials, LLC designs, manufactures, and installs multilayer insulation (MLI) blankets and passive thermal control products. They also fabricate soft goods and ins
Airbus Defence and Space
Airbus Defence and Space designs and manufactures satellites, spacecraft equipment, and provides related services for telecommunications, navigation, Earth observation, and space exploration
Akash Systems
US developer of GaN-on-Diamond satellite radios and power amplifiers delivering 3-5x higher data rates through proprietary Diamond Cooling technology.
Allatherm
Latvian company making heat pipes and loop heat pipes for space thermal management, collaborating with ESA, Airbus D&S, Thales, DLR, and JAXA, and developing a Xenon compressor for ESA Lunar
Arquimea
Spanish space technology company founded 2007 in Leganes, developing MEMS relay switches, SiC power devices, and miniaturized power conditioning units for satellite applications.
Boyd Corporation
US manufacturer of engineered material solutions — sealing, EMI shielding, thermal management, and protection technologies — for aerospace, defense, and other demanding industries.
Calyos
Belgian expert in passive two-phase cooling technologies — heat pipes, loop heat pipes, and pulsating heat pipes — for thermal management in aerospace, defense, and industrial applications.
CAVU Aerospace
CAVU Aerospace designs and manufactures spacecraft avionics, including radiation-tolerant onboard computers, thermal control units, frame grabbers, and flight-proven satellite cameras for sp
DHV Technology
DHV Technology is a Spanish space technology company designing and manufacturing solar panels, electrical power systems, MLI blankets, and solar array drive assemblies for CubeSats and small
DUNMORE
US manufacturer of coated and metallised films (Bristol, PA); MLI thermal blankets and spacecraft thermal management films for satellite and space applications; 50+ years experience.
Glavkosmos
Glavkosmos coordinates international human spaceflight projects, facilitates satellite launches, develops and supplies rocket components, and provides equipment for space crews.
Hemeria
HEMERIA designs, produces, and supplies space systems, vehicles, and defense equipment for commercial, institutional, and scientific customers.
Lidax
Madrid-based aerospace engineering company specialising in opto-mechanical systems, flexible thermal straps, and cryogenic units for space missions.
MAP (Aerospace Coatings)
MAP is a European aerospace surface treatment and coatings company specializing in thermal control coatings, optical solar reflectors, and surface preparation materials for spacecraft and sa
Minco Products, Inc
Minco Products, Inc. designs and manufactures solutions for heating, flex circuits, temperature sensing, and instrumentation. They offer off-the-shelf products and craft customized solutions
Northrop Grumman Space Systems
Minotaur family, Pegasus XL, Antares (legacy); MLV co-development with Firefly.
Paragon Space Development Corporation
US life support and thermal control engineering company providing environmental control systems, spacesuits, and thermal management solutions for NASA, commercial, and defense space programs
Peraton Space
US national security technology company providing satellite communications, space domain awareness, ground systems operations, and intelligence support services to the US government and mili
Pumpkin, Inc.
San Francisco-based manufacturer of flight-proven CubeSat kits, SUPERNOVA nanosatellite buses, and spacecraft power/electronics components, with over 150 kits delivered and dozens of success
RUAG Space
Swiss-Swedish space components manufacturer providing satellite structures, thermal control products, payload electronics, and antennas for commercial and institutional programs.
Sheldahl (Multek Flexible Circuits)
Sheldahl (Multek Flexible Circuits) is a US manufacturer of flexible printed circuits, printed electronics, electronic materials, and aerospace thermal control materials, headquartered in No
SPUTNIX
SPUTNIX is a Russian manufacturer of nanosatellite and microsatellite platforms, onboard subsystems and ground infrastructure, operating as a subsidiary brand of Sitronics Group.
Technology Applications Inc (TAI)
American thermal strap manufacturer founded 1994 in Boulder CO; world's largest maker of flexible thermal links (copper, graphite, PGS); flown on Orion, OSIRIS-REx, Solar Orbiter, and Starli
Thales Cryogenics
Dutch space cryocooler manufacturer in Eindhoven (Thales Nederland); Stirling, pulse tube, and J-T coolers for IR detectors at 10-200K; heritage on XMM-Newton, Herschel, Gaia, INTEGRAL.
Thermal Space Ltd.
US thermal-management engineering firm in Boulder, Colorado, designing and manufacturing spacecraft thermal straps, cold plates, and cryogenic cooling hardware.
Thermavant
US oscillating heat pipe (OHP) thermal management company; heat frames, chassis, radiators, and cold plates for space, airborne, and high-temperature electronics applications.
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