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Match Document Document Title
US20140097981 SATELLITE WITH DEPLOYABLE PAYLOAD MODULES  
A telecommunication satellite with geostationary orbit comprises an upper module, a lower module, and a lateral module, disposed in a storage configuration between the upper module and the lower...
US20120043427 ABSORBENT DOME FOR A RADIATING COLLECTOR TUBE  
The device for thermal monitoring for a piece of equipment, whereby said piece of equipment is integrated on a craft placed in a forced vacuum environment, an outside part (7) of the equipment...
US20120175467 MICROMETEOROID AND ORBITAL DEBRIS (MMOD) AND INTEGRATED MULTI-LAYER INSULATION (IMLI) STRUCTURE  
A micrometeoroid and orbital debris-integrated multi-layer insulation (MMOD/IMLI) structure including at least one ballistic layer, which may be flexible, and at least one insulation layer, which...
US20130181094 ORBIT DEBRIS REMOVAL AND ASSET PROTECTION ASSEMBLY  
An orbital debris removal assembly is provided. The orbital debris removal and asset protection assembly includes a plurality of spaced layers of netting. Each netting layer includes a plurality...
US20120097799 ORBIT DEBRIS REMOVAL AND ASSET PROTECTION ASSEMBLY  
An orbital debris removal assembly is provided. The orbital debris removal and asset protection assembly includes a plurality of spaced layers of netting. Each netting layer includes a plurality...
US20120068018 ORBITAL DEBRIS MITIGATION SYSTEM AND METHOD  
Fiber-based debris interceptors are used to intercept and/or contain space debris. The debris interceptors may be made up of fibers that are formed in space from a material supply on a space...
US20080078884 Deployable heat shield and deceleration structure for spacecraft  
An apparatus for heat shielding and deceleration of a spacecraft comprises an unfoldable shield of individual panels made of a high temperature resistant fiber reinforced ceramic and pivotally...
US20150259081 INTEGRATED ARMOR FOR HYPERVELOCITY IMPACTS  
Apparatus and methods described herein provide for a structural armor configured to provide load-bearing capabilities to a structure, as well as to provide protection from hypervelocity impacts....
US20110198446 Device for Eliminating Space Debris in Orbit  
A device for eliminating space debris in orbit, the device including a covering that when struck by an object of space debris breaks this up into multiple pieces of predetermined size, and...
US20050230560 ESD coatings for use with spacecraft  
Spacecraft with electrostatic dissipative surfaces are disclosed herein. The surface has layer which includes a plurality of carbon nanotubes to incorporate electrical conductivity into space...
US20120080562 LANDING DEVICE FOR A SPACE PROBE, AND LANDING METHOD FOR A PROBE PROVIDED WITH SUCH A DEVICE  
A space probe including a descent module with a mobile exploration vehicle, wherein the descent module is a landing module inside which the mobile exploration vehicle is fastened, the landing...
US20060060718 Radiation shield  
A radiation shield for use with a manned spacecraft is claimed. The shield has a container that is substantially filled with a substantially radiation absorbing material. The container has...
US20090108137 PRESSURE VESSEL HAVING CONTINUOUS SIDEWALL  
A spacecraft pressure vessel has a tub member. A sidewall member is coupled to the tub member so that a bottom section of the sidewall member extends from an attachment intersection with the tub...
US20110005382 Methods and structures for sandwich panels with improved resistance to ballistic penetration  
Provided herein methods and structures for construction of light weight sandwich panels or load-bearing panels having improved ballistic protection. The methods disclosed can facilitate...
US20080048069 Uncoupled vibrion attenuation/isolation devices  
The present invention relates to a vibration attenuation/isolation device. An implementation of the invention provides an improved whole-spacecraft vibration attenuation/isolation by separating...
US20140239124 SPACECRAFT WITH OPEN SIDES  
A spacecraft may include a module structure having a plurality of module sides. The spacecraft may include a central cylinder extending through a center of the spacecraft. The central cylinder may...
US20120091280 CRYOGENIC PROPELLANT DEPOT AND INTEGRAL SUNSHIELD  
A cryogenic propellant depot and sunshield are provided for operation in earth orbit to fuel or refuel other space vehicles. The sunshield is deployed to effectively mitigate solar radiation...
US20090084903 Spacecraft Having A Magnetic Space Radiation Shield  
There is provided a radiation shield device for providing radiation protection to an area, such as a spacecraft including, for example, a manned vehicle. The radiation shield device comprises a...
US20120091281 CRYOGENIC PROPELLANT DEPOT AND DEPLOYABLE SUNSHIELD  
A cryogenic propellant depot and sunshield are provided for operation in earth orbit to fuel or refuel other space vehicles. The sunshield is deployed to effectively mitigate solar radiation...
US20120001027 TRANSPARENT CERAMIC COMPOSITE  
A ceramic composite and method of making are provided. The ceramic composite may be transparent and may serve as transparent armor. The ceramic portion of the composite may be spinel. The...
US20120160966 CNT-TAILORED COMPOSITE SPACE-BASED STRUCTURES  
An apparatus having a composite space-based structure with a first carbon nanotube infused material and a second carbon nanotube infused material. The first and second carbon nanotube infused...
US20120318928 Spacecraft magnetic shield  
A spacecraft magnetic shield apparatus is disclosed. One embodiment has an armature attached at one end of a spacecraft and an electromagnet attached to the other end. A computer determines the...
US20090065647 SOLAR PROTECTION DEVICE FOR SPACE INSTRUMENT  
The present invention relates to a solar protection device for space instrument. This invention is particularly suited to electromagnetic measuring instruments pointing in a direction close to...
US20130037656 UTILIZATION OF AN ENHANCED ARTIFICIAL MAGNETOSPHERE FOR SHIELDING AGAINST SPACE ENVIRONMENTAL HAZARDS  
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...
US20090084902 THERMAL PROTECTION SYSTEM WITH STAGGERED JOINTS  
The thermal protection system disclosed herein is suitable for use with a spacecraft such as a reentry module or vehicle, where the spacecraft has a convex surface to be protected. An embodiment...
US20110049303 SPACECRAFT SHIELD  
A spacecraft is described which uses a magnetic field source to generate a shield magnetic field to protect the spacecraft from energetic charged particles. The field may be perturbed to increase...
US20050151021 Heat dissipating, light-reflecting plates for radiator systems of spacecraft and methods for fabricating the same  
A heat-dissipating, light-reflecting plate for a radiator of a spacecraft is provided. The heat-dissipating, light-reflecting plate has an at least partially transparent, thermally conductive...
US20100187364 CRYOGENIC PROPELLANT DEPOT AND INTEGRAL SUNSHIELD  
A cryogenic propellant depot and sunshield are provided for operation in earth orbit to fuel or refuel other space vehicles. The sunshield is deployed to effectively mitigate solar radiation...
US20100187365 CRYOGENIC PROPELLANT DEPOT AND DEPLOYABLE SUNSHIELD  
A cryogenic propellant depot and sunshield are provided for operation in earth orbit to fuel or refuel other space vehicles. The sunshield is deployed to effectively mitigate solar radiation...
US20130062472 Apparatus for Spacecraft  
The invention relates to the protection of spacecraft from debris and to de-orbiting devices of the atmospheric drag type, and to debris sweeping apparatus for the removal of debris from the space...
US20150225093 Combined Pressure and Thermal Window System for Space Vehicles  
A window system for a vehicle comprising a pressure and thermal window pane, a seal system, and a retainer system. The pressure and thermal window pane may be configured to provide desired...
US20120090658 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...
US20100132915 Cooling System for Aerospace Vehicle Components  
A cooling system for removing heat generated by electrical components onboard aerospace vehicles flows coolant between an evaporator that removes heat from the component, and a condenser within...
US20120267482 Device for Protecting an Optical Instrument of a Satellite  
A device for protecting an optical instrument of a satellite comprises a body on which the optical instrument is mounted, said protection device having a folded-down position and a deployed...
US20120273622 MULTIFUNCTIONAL CHAMBERED RADIATION SHIELDS AND SYSTEMS AND RELATED METHODS  
Radiation shields include an outer composite wall, an inner composite wall, and an enclosed fuel chamber disposed between the inner and outer composite walls. A fuel may be contained within the...
US20110260007 SPACE PROBING APPARATUS  
A space probing apparatus is provided that can further enhance its thermal protective function for electronic apparatuses and batteries that are apparatuses each having a narrow range of...
US20170121038 SYSTEMS AND METHODS FOR SHIELDING STRUCTURES FROM RADIATION AND MAGNETIC FIELD EXPOSURE  
A system is configured to shield an interior chamber of a structure. The system may include a power source, an outer shield assembly operatively connected to the power source and coupled to an...
US20170113777 Structural Arrangement, Aircraft Or Spacecraft, And Method For Producing A Structural Arrangement  
A structural arrangement for an aircraft or spacecraft, in particular a fuselage structural arrangement, is disclosed. The structural arrangement includes: a former; a metal skin; and a fibre...
US20170093483 HYBRID COMMUNICATIONS ASSEMBLY FOR SPACECRAFT  
A hybrid communications assembly for a spacecraft is provided. The hybrid communications assembly may include an assembly base, one or more laser communications terminals mounted on the assembly...
US20170093004 HIGH-FREQUENCY CAVITY RESONATOR FILTER WITH DIAMETRICALLY-OPPOSED HEAT TRANSFER LEGS  
A heat transfer interface is provided for radio-frequency resonator cavity filters used in vacuum environments such as are encountered by spacecraft and satellites. The heat transfer interface may...
US20170036786 Passive Thermal System Providing an Embedded Interface for Heat Pipes  
A passive thermal system for use in aerospace vehicles includes a first passive thermal panel having at least one internal resident heat pipe, wherein the first passive thermal panel is further...
US20160376039 HEAT SHIELD FOR A SPACECRAFT  
Various material compositions of a heat shield for a spacecraft are described. The heat shield can be formed by multi-dimensional weaver or three-dimensional (3-D) printer. Furthermore, the heat...
US20160362199 STAND-OFF PANEL THERMAL PROTECTION SYSTEM AND METHOD OF FABRICATING THE SAME  
A stand-off panel thermal protection system is disclosed. The system comprises a sandwich panel comprising: a first ceramic matrix composite facesheet and a second ceramic matrix composite...
US20160297552 Deployable Device for the Thermal Insulation of Cryonic Tanks of Spacecraft  
In a deployable device for the thermal insulation of cryogenic tanks (2) of spacecraft (1), including at least one insulating mat (8), preferably a plurality of insulating mats (8) distributedly...
US20160297551 RADIATOR WITH REDUCED INSOLATION FOR SATELLITE AND SATELLITE PROVIDED WITH SUCH A RADIATOR  
A radiator for a satellite intended for being placed in geostationary orbit around the earth in a tilted plane relative to the plane of the ecliptic, includes at least one panel having at least...
US20160288928 Passive Thermal System Comprising Combined Heat Pipe and Phase Change Material and Satellites Incorporating Same  
A passive thermal system for use in a satellite and other aerospace applications includes a container having a heat-pipe working fluid disposed in a first chamber and a Phase Change Material (PCM)...
US20160200460 SPACECRAFT AND SPACECRAFT PROTECTIVE BLANKETS  
Protective blankets include a plurality of sheets of material operatively coupled together to define the protective blanket. The plurality of sheets includes at least one sheet composed of carbon...
US20160194096 CLIMATE- REGULATING- SYSTEM  
For many millennia's Earth has had an active and very effective process of controlling-limiting earth climate factors that have fostered the evolution of many varieties of life forms in both...
US20160167811 Multi-Layered Self-Healing Material System Towards Impact Mitigation  
Various embodiments provide multi-layered self-healing materials, capable of repairing puncture damage. The multi-layered self-healing materials, capable of repairing puncture damage of the...
US20160152355 Apparatus For Spacecraft  
The invention relates to the protection of spacecraft from debris and to de-orbiting devices of the atmospheric drag type, and to debris sweeping apparatus for the removal of debris from the space...

Matches 1 - 50 out of 55 1 2 >