Patents for B64G 1 - Cosmonautic vehicles (11,089)
03/2011
03/03/2011US20110049303 Spacecraft shield
03/03/2011US20110049302 Retro-Geo Spinning Satellite Utilizing Time Delay Integration (TDI) for Geosynchronous Surveillance
03/03/2011DE102010029684A1 Antrieb, insbesondere für Raumfahrzeuge Drive, in particular for spacecraft
03/03/2011CA2717136A1 Biased releasable connection system
02/2011
02/24/2011WO2010126604A3 Terminator tape satellite deorbit module
02/24/2011US20110042522 Robust capacitive distance sensor
02/24/2011US20110042521 Spacecraft Launch and Exploration System
02/24/2011US20110042386 Pressure vessel for propellants, explosion preventing method of the same, and manufacturing method of the same
02/23/2011EP2287933A2 Heat pump for high temperature environments
02/23/2011EP2287075A2 Multi-axis articulated solar light shade for space-based sensors
02/23/2011EP2285868A1 Thioethers, methods for their preparation, and compositions including such thioethers
02/22/2011US7893390 Guided missile
02/17/2011WO2011019830A1 Electrostatic spacecraft reorbiter
02/17/2011WO2010141121A3 Locking device with a shape memory alloy actuator and method of use
02/17/2011US20110036953 Methods and apparatus for an integrated instrumentation module for a thermal protection system
02/17/2011US20110036952 Electrostatic Spacecraft Reorbiter
02/17/2011US20110036951 Hybrid electrostatic space tug
02/16/2011EP2282940A1 Method for controlling satellite attitude, and attitude-controlled satellite
02/16/2011CN101977815A Actuator device for varying the attitude of a spacecraft
02/10/2011US20110031352 Two Part Spacecraft Servicing Vehicle System with Adaptors, Tools, and Attachment Mechanisms
02/10/2011DE19923449B4 Flugkörper mit photoelektrischer Umwandlungsvorrichtung Missiles with photoelectric conversion device
02/10/2011DE102009036518A1 Aerospace missile, has actuator coupled with engines in such manner that control unit operates actuator for pivoting engines during change of assigned angle and resulting thrust in direction of thrust axis
02/10/2011DE102009036327A1 Fluid-dynamic actuator for controlling position of small satellite, has transformer and frequency producing element electrically connected to each other such that electrical voltage of spacecraft is transformed into direct current voltage
02/09/2011CN101508525B Process for producing cerium doped secondary surface polished plate glass substrate for spaceflight
02/03/2011US20110024572 Device for reducing aerodynamic drag
02/03/2011US20110024571 Gyroless transfer orbit sun acquisition using only wing current measurement feedback
02/03/2011US20110024548 Launching system and launching apparatus
02/03/2011DE102009035265A1 Druckrumpf eines Luft- oder Raumfahrzeuges mit Druckkalotte Pressure hull of an aircraft or spacecraft with pressure cap
02/02/2011EP2279947A1 Gyroless transfer orbit sun acquisition using only wing current measurement feedback
02/02/2011EP2279945A2 Launching system and launching apparatus
02/02/2011EP2279120A2 Fixing device for the assembly and quick release of objects
02/02/2011CN101965293A Device for detecting space objects
02/01/2011US7878456 Protective shield assembly for space optics and associated methods
01/2011
01/27/2011WO2010141111A3 Multiple-use rocket engines and associated systems and methods
01/27/2011US20110022309 Method for Determining the Position of a Spacecraft with the Aid of a Direction Vector and an Overall Spin Measurement
01/27/2011US20110017875 Photovoltaic array
01/27/2011US20110017874 Means of fuel and oxidizer storage
01/27/2011US20110017872 Sea landing of space launch vehicles and associated systems and methods
01/26/2011CN101383568B Synchronous expansion mechanism for foldable inflating expansion solar cell paddles
01/25/2011US7875838 Post boost control power assembly
01/25/2011US7874520 Satellite with deployable, articulatable thermal radiators
01/25/2011US7874519 Spacecraft three-axis attitude acquisition from sun direction measurement
01/20/2011WO2011008136A1 Spacecraft for interplanetary and intergalactic flight
01/20/2011WO2011008134A1 Method for propelling a spacecraft at supercosmic speeds
01/20/2011WO2010112764A3 Device for separating the two portions of a launcher refueling module
01/20/2011US20110011983 Multijunction photovoltaic cell grown on high-miscut-angle substrate
01/20/2011US20110011982 Modular control moment gyroscope (cmg) system for spacecraft attitude control
01/19/2011EP2275348A2 Segmented parabolic concentrator for space electric power
01/19/2011CN101948011A Hexapod universal walking multifunctional moonshot robot
01/13/2011WO2011005422A2 Sea landing of space launch vehicles and associated systems and methods
01/13/2011WO2011003965A2 Device for gentle linear separation of a first part and a second part
01/13/2011US20110010027 Systems and methods for attitude propagation for a slewing angular rate vector
01/13/2011US20110006163 Segmented parabolic concentrator for space electric power
01/13/2011US20110006162 Actuator device for varying the attitude of a spacecraft
01/13/2011US20110005382 Methods and structures for sandwich panels with improved resistance to ballistic penetration
01/13/2011US20110005192 Cooling system for an aircraft, aircraft comprising the cooling system and cooling method
01/12/2011EP2272761A1 Extendable structure
01/12/2011EP2165433B1 System for positioning a terrestrial user
01/12/2011EP2038104B1 Assembly of prepregs for producing structures, for example ones which deploy through inflation
01/12/2011CN201703569U Installation and storage platform for equipment of space station
01/12/2011CN201703568U Wheel leg combined bionic lunar rover
01/12/2011CN201703567U Wheel leg structure
01/12/2011CN101943082A Heating gasification device for liquefied gas micro-propulsion system
01/12/2011CN101941530A Cargo carrying auxiliary device for outer space
01/12/2011CN101941529A Layout method for micro attitude and orbit control thruster array
01/12/2011CN101941528A Flywheel based attitude maneuvering control device and method for successive approaching of satellite rounding instantaneous Euler shaft
01/12/2011CN101941527A Multi-sensor integrated attitude determining system structure
01/12/2011CN101941526A Horizontal oscillating bar four-wheel rover
01/11/2011US7866607 Piggyback satellite payload arrangement, a device for and method of attaching a piggyback satellite payload and adapter to be used for a piggyback satellite payload arrangement for launching the piggyback satellite
01/11/2011CA2479566C Control moment gyro for attitude control of a spacecraft
01/06/2011US20110001013 Spacecraft modular thermal platform
01/05/2011EP2270679A1 Method for optimal control of a system which can be modelled by Hamilton-Jacobi-Bellman equations
01/05/2011CN101938076A Microsatellite unplugged cable network
01/05/2011CN101934863A Satellite posture all-round controlling method based on magnetic moment device and flywheel
01/05/2011CN101537770B Probe vehicle wheel with variable diameter elastically capable of automatic extension
01/05/2011CN101513939B Two dimentional attitude control system of synthetic aperture radar satellite
01/04/2011US7861976 Latching separation system
01/04/2011US7861975 Two part spacecraft servicing vehicle system with universal docking adaptor
01/04/2011US7861974 Docking system
12/2010
12/30/2010US20100327119 Satellite communication system, infrastructure and method of providing same
12/30/2010US20100327108 Spacecraft afterbody device
12/30/2010US20100327107 Bidirectional control surfaces for use with high speed vehicles, and associated systems and methods
12/30/2010US20100327106 System and Method for Attitude Control of a Flight Vehicle using Pitch-Over Thrusters
12/30/2010US20100326045 Multiple-use rocket engines and associated systems and methods
12/29/2010WO2010135421A8 Attitude control system for small satellites
12/29/2010CN101927838A Space toilet
12/29/2010CN101927837A Universe light station stereo network system
12/29/2010CN101927836A Aerospace vehicle laser light sail engine
12/29/2010CN101314411B Shielding surface apparatus with space capable of being expanded
12/28/2010US7857261 Docking system
12/23/2010WO2010148025A1 Compensating for wind prior to engaging airborne propulsion devices
12/23/2010WO2010148023A1 Predicting and correcting trajectories
12/23/2010WO2010146126A1 Extendable structure
12/23/2010US20100320330 Control moment gyroscope based momentum control systems in small satellites
12/23/2010US20100320329 Launch vehicles with fixed and deployable deceleration surfaces, and/or shaped fuel tanks, and associated systems and methods
12/23/2010US20100319270 Extendable structure
12/23/2010CA2765616A1 Extendable structure
12/22/2010EP2264317A1 Two-phase heat-exchange method and device with bearing-mounted gear pump
12/22/2010EP2263938A2 Cooling device for effusion or transpiration cooling
12/22/2010EP2263937A1 Control moment gyroscope based momentum control systems in small satellites
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