Patents for B64G 1 - Cosmonautic vehicles (11,089)
08/1994
08/23/1994US5339623 Singly fueled multiple thrusters simultaneously energized by a common power supply
08/23/1994US5339574 Inflatable mold construction
08/23/1994CA1331596C Spacecraft with increased stationkeeping fuel load
08/18/1994WO1994018073A1 Autonomous on-board satellite control system
08/18/1994DE4304129A1 Device and method for producing a linear movement and a rotational movement by means of changes in rotational pulses
08/16/1994US5337981 Method and apparatus for compensating for solar torque transients on a satellite during a solar eclipse
08/16/1994US5337980 Spacecraft-to-launch-vehicle transition
08/09/1994US5337288 Acoustic and vibration attenuation composite material
08/09/1994US5337241 Spacecraft attitude sensor having an optical apparatus for increasing applications thereof
08/09/1994US5335720 Heat pipe
08/04/1994WO1994017427A1 Sensor for detecting the intensity and angle of incidence of solar radiation
08/03/1994EP0608945A1 Star sensor with CCD-array, method of detection and application to reposition a spacecraft
08/02/1994US5335179 Unified spacecraft attitude control system with pseudo-complementary paired thrusters
08/02/1994US5334965 Superconductive material and magnetic field for damping and levitation support and damping of cryogenic instruments
08/02/1994US5334848 Spacecraft docking sensor system
08/02/1994US5333964 Slip joint connector
08/02/1994US5333819 Self tuning motion/vibration suppression system
07/1994
07/26/1994US5332187 Adjusting arrangement
07/26/1994US5332030 Multi-directional cooler
07/21/1994WO1994016286A1 Control device
07/21/1994WO1994015834A1 Spacecraft power bus regulation using solar panel position
07/19/1994US5330124 Thermal protection device using the vaporization and superheating of a rechargeable liquid
07/19/1994US5329762 Method for assembling rocket propulsion motor
07/13/1994CN1089225A Frangible joint separation system
07/12/1994US5328312 Dual load-path fastener
07/12/1994US5328132 Engine protection system for recoverable rocket booster
07/07/1994WO1994014654A1 Gyro nutation damper
07/07/1994WO1994014653A1 Direct torque control moment gyroscope
07/06/1994EP0605027A1 Image processing device for estimating the parameters of an ellipse and identifying its centre
07/06/1994EP0604588A1 Waste-water treatment system
07/05/1994US5326186 Robot friendly probe and socket assembly
07/05/1994US5326054 Apogee at constant time-of-day equatorial (ACE) orbit
06/1994
06/29/1994EP0604214A2 A spacecraft having east/west orbit control during a north or south stationkeeping manoeuvre
06/29/1994EP0603869A1 Magnetic torque attitude control system
06/29/1994EP0603521A1 Oil cooler for spacecraft
06/29/1994EP0364569B1 Rocket-powered, air-deployed, lift-assisted booster vehicle for orbital, supraorbital and suborbital flight
06/28/1994US5323682 Heat resistant covering
06/23/1994DE4342073A1 Exterior insulation for pipe contg. liquid hydrogen at very low temp.
06/23/1994DE4243562A1 Payload-extension system from spacecraft
06/23/1994DE4242977A1 Container with flexible outer walls for holding fluid material
06/22/1994EP0603058A1 Method for controlling the attitude of a satellite directed towards a celestial object and a satellite for implementing the same
06/22/1994EP0602668A1 Propellant immobilizing method
06/21/1994US5323317 Method and apparatus for determining runoff using remote geographic sensing
06/21/1994US5322725 Thermal protection system
06/21/1994US5322248 Methods and arrangements tailoring aerodynamic forces afforded by a payload to reduce flight loads and to assist flight control for the coupled system
06/18/1994CA2111602A1 Method for controlling the attitude of a satellite aimed towards a celestial object and a satellite suitable for implementing it
06/15/1994EP0601544A1 Dark current compensation of pixels tracking stars several times
06/15/1994EP0601061A1 Three-axis stabilized, earth oriented satellite and corresponding sun and earth acquisition device-------------------------------.
06/15/1994EP0601051A1 Measurement arrangement useful for controlling the attitude of a three-axis stabilized satellite, corresponding evaluation process, regulating system and process.
06/14/1994US5321336 Device for removing a negative charge from a body
06/14/1994US5320395 Microconical interface fitting and interface grasping tool
06/14/1994US5319969 Method for determining 3-axis spacecraft attitude
06/14/1994US5319968 Apparatus for determining 3-axis space craft attitude
06/14/1994US5319926 Thruster for spacecraft
06/14/1994US5319905 Panel array deployment apparatus
06/08/1994EP0600786A1 Automatic charging device for a furnace in space
06/07/1994US5318256 Rocket deceleration system
06/07/1994US5318255 Stage separation mechanism for space vehicles
06/07/1994US5318108 Gas-controlled dynamic vacuum insulation with gas gate
06/07/1994CA1330071C Rocket-powered, air-deployed, lift-assisted booster vehicle for orbital, supraorbital and suborbital flight
06/02/1994CA2110358A1 Loader device for an automatic furnace in space
05/1994
05/31/1994US5315888 Gyro nutation damper
05/31/1994CA2013332C Collapsible truss structures
05/26/1994WO1994011249A1 Waveguide absorber
05/24/1994US5315158 For a missile
05/24/1994US5314146 Multi-mission spacecraft bus having space frame structural design
05/24/1994US5313851 Reusable mass propulsion system
05/24/1994CA2013632C Antenna pointing device
05/24/1994CA1329691C Self-motorized antifriction joint and an articulated assembly, such as a satellite solar panel, equipped with such joints
05/19/1994DE4337968A1 Coupling mechanism extending and interlocking space vehicle elements - has hinged links secured together by latch element subjected to spring loading to maintain position
05/18/1994EP0597750A1 Apparatus for holding and ejecting an object relative to a support following a controlled sequence
05/18/1994EP0597240A1 Injection device and process
05/18/1994EP0596886A1 Space transport architecture and method for robotic planetary operations
05/17/1994US5312693 Nonsacrificial laser hardening
05/17/1994US5312685 Atomic oxygen protective coating with resistance to undercutting at defect sites
05/17/1994US5312152 Shape memory metal actuated separation device
05/17/1994US5312073 Method for controlling the pitch attitude of a satellite by means of solar radiation pressure and satellite, in particular an electric propulsion satellite, suitable for implementation of the method
05/11/1994WO1994010036A1 Device with two gyroscopes for swivelling a flying object
05/11/1994EP0596821A1 Coating for thermal insulation material containing mineral fibres and process for manufacturing the same
05/11/1994EP0596779A1 Method and system for protecting an oxidizable material against oxidation
05/11/1994EP0596400A2 Frangible annular joint for connecting and disconnecting two elements
05/10/1994US5311435 Method for station keeping control of flexible spacecraft using onboard gain scheduling scheme
05/10/1994US5311022 Tri-scan horizon sensor
05/10/1994US5310144 Method and apparatus for satellite torque balancing
05/10/1994US5310143 Three axis thruster modulation
05/10/1994US5310141 Battery thermal control arrangement
05/05/1994DE4337581A1 System zur Versorgung von Motoren eines Raumfahrzeuges mit flüssigem Treibstoff System for the supply of engines of a spacecraft with liquid fuel
05/05/1994DE4316247A1 Vacuum glider Alpha with three-part structure - which is determined by quadrant, its circumscribed circle, rectangular, isosceles triangle, and isosceles triangle
05/05/1994CA2102480A1 Optimized system for feeding a reignitable rocket engine
05/05/1994CA2082097A1 Stirrup assembly for securing a cargo having upper and lower pairs of opposed, ball headed studs extending laterally from each side of a cylindrical, securing stud
05/03/1994US5309529 Bearing arrangement for a radial bearing in an acceleration-proof gyroscope
05/03/1994US5308366 Exothermic reaction of beryllium and oxygen, spacecraft
05/03/1994US5308025 Spacecraft spin axis capture system and method
05/03/1994US5308024 Attitude control system
05/03/1994CA1329246C Transition control system for spacecraft attitude control
04/1994
04/28/1994WO1994009333A1 Dynamic vacuum insulation
04/28/1994DE4336044A1 Articulated connection for individual elements of folding structure - has two cable pulleys and cam disc with drive transfer devices for simultaneous coordinated rotation
04/28/1994DE4243273A1 Einrichtung zum Schwenken eines Flugkörpers, mit zwei Kreiseln Means for pivoting a missile with two rotors
04/26/1994US5305981 Multiaxis vibration isolation system
04/26/1994US5305974 Spaceship propulsion by momentum transfer
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