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67results about "Spacecraft coatings" patented technology
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Polymeric coating for protecting objects
ActiveUS8053492B2Provide protectionCosmonautic power supply systemsCosmonautic thermal protectionSilsesquioxanePhenyl group
A protective polymeric coating is applied to the surface of various objects which are to be exposed to a harsh environment. The protective polymeric coating covers the exposed surface, where the polymeric coating includes a polyimide polymer. The polyimide polymer in the polymeric coating has a backbone with at least one non-terminal phenyl group. A linkage is connected to the non-terminal phenyl group, where the linkage can be an amide linkage or an ester linkage. An oligomeric silsesquioxane compound is connected to the linkage through an organic substituent, where the oligomeric silsesquioxane is not incorporated into the polymer backbone. The polymeric coating provides protection to the underlying object.
Owner:NEXOLVE HLDG CO LLC
Thioethers, methods for their preparation, and compositions including such thioethers
Disclosed are thioethers, methods for preparing such thioethers, and curable compositions, such as coating and sealant compositions, that include such thioethers. The thioethers can be the reaction product of (a) an alpha, omega dihalo organic compound, (b) a metal hydrosulfide, and (c) a metal hydroxide.
Owner:PRC DE SOTO INT INC
Thermal insulating coating for spacecrafts
InactiveUS6939610B1Minimize temperature gainIncrease energy densityFireproof paintsCosmonautic vehiclesHeat storage materialPhase change
To protect spacecraft and their contents from excessive heat thermal protection systems are essential. For such thermal protection, metal coatings, ceramic materials, ablative materials, and various matrix materials have all been tried, but none have been found entirely satisfactory. The basis for this thermal protection system is the fact that the heat required to melt a substance is 80 to 100 times larger than the heat required to raise its temperature one degree. This led to the use herein of solid-liquid phase change materials. Unlike conventional heat storage materials, when phase change materials reach the temperature at which they change phase they absorb large amounts of heat without getting hotter. By this invention, then, a coating composition is provided for application to substrates subjected to temperatures above 100° F. The coating composition includes a phase change material.
Owner:NASA
Polymeric coating for the protection of objects
ActiveUS8309627B2Provide protectionCosmonautic vehiclesCosmonautic radiation protectionSilsesquioxaneLinkage concept
Owner:NEXOLVE HLDG CO LLC
Lightning protection sheet with patterned discriminator
ActiveUS20100264665A1Improve conductivityLow conductivityTyre partsFuselage bulkheadsDiscriminatorEngineering
A lightning protection system is provided, typically for use on an outer surface of an aircraft, which includes the use of a lightning protection sheet that includes an electrically conductive film and at least one patterned, electrically non-conductive discriminator layer.
Owner:3M INNOVATIVE PROPERTIES CO
Durable refractory ceramic coating
Owner:ECESIS
Material for thermally loaded substrates
InactiveUS6821656B2Avoid overall overheatingReduce mechanical stressPropellersMolten spray coatingThermal insulationLanthanide
The invention relates to a material, in particular for a thermal insulation layer, with increased thermal stability, a low heat conductivity and a large thermal coefficient of expansion. According to the invention, said material comprises lanthanides, in particular the elements La, Ce, Nd, Yb, Lu, Er or Tm, which preferably occur as a mixture in a Perovskite structure. Said thermal insulation layer is particularly suitable for replacing thermal insulation layers comprising yttrium stabilized zirconium oxides (YSZ) as the thermal stability thereof is given as well over 1200° C.
Owner:FORSCHUNGSZENTRUM JULICH GMBH
Mixed germanium-silicon thermal control blanket
ActiveUS7270891B2Cosmonautic environmental control arrangementCosmonautic radiation protectionElectrostatic dischargeMaterials science
Owner:NORTHROP GRUMMAN SYST CORP
Anti-contamination coated multi-layer insulation
ActiveUS7252890B1Reduce presenceImprove efficiencySynthetic resin layered productsCosmonautic thermal protectionSolar absorptanceUltraviolet
A multi-layer insulation (MLI) blanket with enhanced contamination inhibiting properties and a method for inhibiting the formation of organic residues on the outer surface of a MLI blanket are provided. In one embodiment, a MLI blanket (10) attachable to a spacecraft or other structure includes a plurality of metallized layers (20, 30, 40, 50) separated by mesh layers (60, 62, 64). An anti-contamination coating (80) comprised of a photocatalytic material is disposed between a high emittance layer (70) that overlies the outer surface (20A) of the outer metallized layer (20) and an outer electrically conductive layer (90). When exposed to ultraviolet or near-ultraviolet radiation components present in solar radiation, the anti-contamination coating (80) catalyzes the breakdown of organic residues on the outer surface of the MLI blanket (10) thereby maintaining the reflective properties of the MLI blanket (10) and ensuring that solar absorptance of the MLI blanket (10) is maintained at or below an acceptable threshold level.
Owner:LOCKHEED MARTIN CORP
Durable refractory ceramic coating
Owner:ECESIS
Material for thermally loaded substrates
The invention relates to a material, in particular for a thermal insulation layer, with increased thermal stability, a low heat conductivity and a large thermal coefficient of expansion. According to the invention, said material comprises lanthanides, in particular the elements La, Ce, Nd, Yb, Lu, Er or Tm, which preferably occur as a mixture in a Perovskite structure. Said thermal insulation layer is particularly suitable for replacing thermal insulation layers comprising yttrium stabilised zirconium oxides (YSZ) as the thermal stability thereof is given as well over 1200° C.
Owner:FORSCHUNGSZENTRUM JULICH GMBH
Lightweight protector against micrometeoroids and orbital debris (MMOD) impact using foam substances
Methods and apparatus are provided for a shield to protect a surface from the impact of hyper-velocity projectiles. The apparatus comprises a foam material that is configured to cover the surface to be protected and is attached directly to that surface. A coating material is typically disposed on the outer surface of the foam material and may penetrate the foam material to a predetermined depth. The foam material and the coating material are selected to form a composite having predetermined values of sonic velocity, toughness, and thermal conductivity. The composite of foam material and coating material can be significantly lighter in weight than a metal shield having equivalent protective characteristics.
Owner:THE BOEING CO
Utilization of an enhanced artificial magnetosphere for shielding against space environmental hazards
InactiveUS20130037656A1Enhances artificial magnetosphereReduce exposureCosmonautic vehiclesCosmonautic radiation protectionX-rayElectromagnetic shielding
This invention relates to technology used for creating an enhanced artificial magnetosphere or electromagnetic shield for use in both manned and unmanned spacecraft. The invention includes an Interference Generating Pattern (IGP) which is tuned to the high-frequency radiation of X-rays and gamma rays and a conformal magnetic field. This technology will reduce the exposure of astronauts or other space travelers, as well as radiation-sensitive equipment, to the environmental hazards present therein. The net result will be reduced radiation intensity in order to create a space radiation-free environment as to render space travel safe.
Owner:INTEGRAL ELECTROMAGNETRONIC TECH
Lightning protection sheet with patterned discriminator
Owner:3M INNOVATIVE PROPERTIES CO
Multi-functional protective assemblies, systems including protective assemblies, and related methods
A protective assembly comprises a first region formulated and configured to provide protection from alpha, beta, and electromagnetic radiation and comprising a composite of particles and polymer; a second region formulated and configured to provide protection from ballistic impact and comprising a composite of fibers and polymer; and a third region formulated and configured to provide protection from thermal radiation and comprising a composite of particles, fiber, and polymer. The protective assembly may be provided on an aerospace structure. The protective assembly may be formed on the aerospace structure body using a co-curing process.
Owner:NORTHROP GRUMMAN SYST CORP
Technological field
A coated structure is provided that has a highly concentrated coating of carbon nanotubes so as to provide integrated thermal emissivity, atomic oxygen (AO) shielding and tailorable conductivity to the underlying surface, such as the surface of an aerospace vehicle, a solar array, an aeronautical vehicle or the like. A method of fabricating a coated structure is also provided in which a surface is coated with a coating having a relative high concentration of carbon nanotubes that is configured to provide integrated thermal emissivity, AO shielding and tailorable conductivity to the surface.
Owner:THE BOEING CO
Coating for prevention of electrostatic discharge within an equipment in a spatial environment
InactiveUS20060169844A1Prevent electrostatic dischargeReduce potential differenceCosmonautic vehiclesCosmonautic power supply systemsPotential differenceEngineering
A solar panel (3) having a front face (31) for receiving solar radiation and a rear face (32), for use in a spacecraft (1). The solar panel is covered on the rear face (32) with a coating (4) having negative electric charge emissive property such that in use the coating expels electrons out of the rear face (32) of the solar panel (3), thus reducing the potential difference between the front face (31) and the rear face (32). A method of reducing potential difference between the front face (31) and the rear face (32) of the solar panel (3) by covering the rear face by said coating (4).
Owner:THALES SA
Directional and areal thermal control coating, using aligned metal oxide mesostructures
InactiveUS7794828B1Easy to scaleCosmonautic environmental control arrangementLayered productsConductive materialsSelf assembling
A thermal control coating derived from a sol-gel process includes a plurality of self-assembled mesopores (and / or mesotubes). The plurality of self-assembled mesopores are aligned with respect to a substrate and / or filled with a conductive material. The aligned and / or filled pores are used to provide thermal control for the substrate having a thermal characteristic.
Owner:HRL LAB
Solid state thermochromic device, and method for producing said device
ActiveUS20190243036A1Reducing solar absorptivityLow costCosmonautic vehiclesMirrorsThermochromismConductive materials
A solid-state thermochromic device and method for producing the device, the device including: a stack successively including, from a rear face to a front face exposed to solar radiation: a) a solid substrate of an inorganic material resistant up to a temperature of 550° C.; b) an infrared-reflective layer of an electronically conductive material; c) electronically insulating interface layers; d) an electronically insulating inorganic dielectric layer transparent to infrared radiation, of cerium oxide CeO2, with a thickness between 400 and 900 nm; e) electronically insulating interface layers; f) a layer of an infrared-active thermochromic material, an n-doped VO2 vanadium oxide, and crystallized in a monoclinic or rutile phase, with a thickness between 30 and 50 nm; and g) a solar-protective coating, transparent to infrared radiation.
Owner:COMMISSARIAT A LENERGIE ATOMIQUE ET AUX ENERGIES ALTERNATIVES +1
Anti-contamination coated multi-layer insulation
ActiveUS7691452B1Reduce presenceImprove efficiencyRadiation applicationsSynthetic resin layered productsSolar absorptanceUltraviolet
A multi-layer insulation (MLI) blanket with enhanced contamination inhibiting properties and a method for inhibiting the formation of organic residues on the outer surface of a MLI blanket are provided. In one embodiment, a MLI blanket (10) attachable to a spacecraft or other structure includes a plurality of metallized layers (20, 30, 40, 50) separated by mesh layers (60, 62, 64). An anti-contamination coating (80) comprised of a photocatalytic material is disposed between a high emittance layer (70) that overlies the outer surface (20A) of the outer metallized layer (20) and an outer electrically conductive layer (90). When exposed to ultraviolet or near-ultraviolet radiation components present in solar radiation, the anti-contamination coating (80) catalyzes the breakdown of organic residues on the outer surface of the MLI blanket (10) thereby maintaining the reflective properties of the MLI blanket (10) and ensuring that solar absorptance of the MLI blanket (10) is maintained at or below an acceptable threshold level.
Owner:LOCKHEED MARTIN CORP
Lightweight protector against micrometeoroids and orbital debris (MMOD) impact using foam substances
Methods and apparatus are provided for a shield to protect a surface from the impact of hyper-velocity projectiles. The apparatus comprises a foam material that is configured to cover the surface to be protected and is attached directly to that surface. A coating material is typically disposed on the outer surface of the foam material and may penetrate the foam material to a predetermined depth. The foam material and the coating material are selected to form a composite having predetermined values of sonic velocity, toughness, and thermal conductivity. The composite of foam material and coating material can be significantly lighter in weight than a metal shield having equivalent protective characteristics.
Owner:THE BOEING CO
Radiation reflector and emitter
A multi-layer radiation reflector / emitter includes first and second materials. The first material is transparent to radiation in a wavelength spectrum ranging from approximately 0.2 microns to at last 6 microns. The first material is a self-supporting arrangement of randomized particles having an average dimension in a range of approximately 0.2 microns to approximately 0.4 microns and defining a fill factor of approximately 0.1 to approximately 0.5. The second material reflects radiation having a wavelength greater than approximately 2 microns.
Owner:NASA
Artificial satellite
ActiveCN107873012AShorten the timeLow costCosmonautic environmental control arrangementCosmonautic thermal protectionPower densitySatellite
The invention relates to an artificial satellite comprising an accumulator (62) apt to dissipate heat, at least one radiator (64) able to remove to space the heat dissipated by the accumulator (62), and a piece of equipment (52) that is said to be not very dissipative and that possesses an individual power density per unit area lower than 250 watts / m2, characterised in that it INC.ludes a thermally insulating cover (66) bounding, with said radiator (64), an isothermal interior zone (68) in which temperature is controlled by radiation, said accumulator (62) and said piece of not very dissipative equipment (52) being arranged under said thermally insulating cover (66), and in that said accumulator (62) has an operating range comprised between 0DEG Cand 50DEG Cand, preferably, between 10DEG Cand 30DEG C.
Owner:AIRBUS DEFENCE & SPACE
Mixed germanium-silicon thermal control blanket
ActiveUS20060105196A1Cosmonautic environmental control arrangementCosmonautic radiation protectionMaterials scienceElectrostatic discharge
A passive thermal control blanket and a method for its manufacture, the blanket including a plastic substrate on which is deposited a film that is a homogeneous mixture of silicon and germanium, thereby combining the excellent reflective and electrostatic discharge properties of germanium with the superior adhesion and corrosion resistance properties of silicon. The uniform mixture is preferably obtained by sputtering the two materials simultaneously onto the substrate, using either separate targets, a single mosaic target, or a single composite target.
Owner:NORTHROP GRUMMAN SYST CORP
Atomic Oxygen-Resistant, Low Drag Coatings and Materials
ActiveUS20190210325A1Increasing atomic oxygen resistanceReduce resistanceArtificial satellitesChemical vapor deposition coatingOrbitAtomic oxygen
Coatings and materials that are atomic oxygen resistant and have an atomically smooth surface that can reduce drag are disclosed. The coatings and materials can be used on at least a portion of a spacecraft intended to operate in harsh environments, such as stable Earth orbits at about 100 km to about 350 km.
Owner:SKEYEON INC
Antistatic Coating For Surfaces Made Of Metal Materials And Dielectric Materials Or Of Dielectric Materials Only In Particular Antenna Surfaces And Method Of Application Thereof
InactiveUS20090033573A1Damage structural integrityAffect performanceOther chemical processesAntenna adaptation in movable bodiesMetallic materialsElectrostatic coating
Thin film coating for transferring antistatic characteristics to the surface on which it is placed, in particular antenna surfaces, in order to prevent electrical charge accumulations on it and discharge phenomenon.
Owner:LEONARDO
Lightning protection device and method of producing same
ActiveUS20160006232A1Easy dischargeEffective protectionCosmonautic propulsion system apparatusAircraft lighting protectorsLightningSurface coating
A lightning protection device for placing on a structure for protecting, and including a first coating including at least one layer of conductive paint; and a second coating deposited on the surface coating and including a material that is thermally insulating and electrically conductive.
Owner:ARIANEGRP SAS
Thermal emission structure
InactiveUS20180334269A1Cosmonautic vehiclesHeat storage plantsElectrical conductorThermionic emission
A thermal emission structure capable of exhibiting heat release characteristics reverse to those of a Phase-change material used therein includes a first conductor layer, a dielectric layer on the first conductor layer, and a second conductor layer on the dielectric layer and having a periodic geometry, at least one of the first conductor layer and the second conductor layer comprises a Phase-change material having an electrical conduction property that varies between a high-temperature phase and a low-temperature phase.
Owner:TOYOTA JIDOSHA KK
Radiative surface
InactiveUS20140106164A1Easy to implementEasy to moveVacuum evaporation coatingSputtering coatingConductive polymerEngineering
A radiative surface comprises a film comprising: a semi-interpenetrated or interpenetrated network of a first ion-conducting polymer and of a second electron- and electrochrome-conducting polymer; and an electrolyte for impregnating the network; the film comprising a first face intended to be in contact with the solar radiations, the first face being covered with a first metallic layer in order to reduce the absorptivity of the solar radiations. A method for creating the radiative surface is also provided.
Owner:THALES SA +1
Polymer seaming with diffusion welds
ActiveUS20100055373A1Decreased tear propagationPrevent thermal deformationCosmonautic vehiclesCosmonautic radiation protectionPolymer science
The present invention is a method for seaming a polymeric material. The method involves forming an interface between a plurality of separate polymeric sheets of materials. Next, heat and pressure are applied to facilitate the diffusion of the polymer molecules at the interface. A diffusion weld is made when the polymer molecules diffuse across the interface.
Owner:NEXOLVE
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