Patents for B64G 1 - Cosmonautic vehicles (11,089)
01/2002
01/16/2002EP1171221A2 Spool valve for switching air flows between two adsorption beds
01/15/2002US6339734 Method and apparatus for reducing spacecraft instrument induced jitter via multifrequency cancellation
01/10/2002WO2002002402A1 Method and device for compensating for thermal deformation of a gravity gradient boom on a satellite
01/10/2002US20020003229 Heat control method and heat controller
01/10/2002US20020003193 Safing mode for high momentum states in body stabilized spacecraft
01/10/2002US20020003192 Satellite system and method of deploying same
01/10/2002DE10029768A1 Verfahren zur Positionshaltung von geostationären Satelliten Method for position keeping of geostationary satellites
01/09/2002EP1170539A1 Device for releasably connecting elements with rotational symmetry
01/09/2002EP1170208A2 Thermal control method and device
01/09/2002EP1169618A2 An angular rate and reaction torque assembly
01/08/2002US6336612 Satellite system and method of deploying same
01/08/2002US6336318 Ion thruster having a hollow cathode assembly with an encapsulated heater, and its fabrication
01/03/2002WO2002001287A1 Electrochromic devices
01/03/2002WO2001064509A3 Aerodynamic fairing
01/03/2002US20020000932 Microwave strip transmission lines, beamforming networks and antennas and methods for preparing the same
01/03/2002US20020000496 Linear actuation device for spacecraft and solar generator unfolding systems
01/03/2002US20020000495 Satellite dispenser
01/02/2002EP1168677A2 Optical data bus communication in an artificial satellite
01/02/2002EP1168673A2 Beam laydown for hopped satellite downlink with adaptable duty cycle
01/02/2002EP1167997A1 Device for measuring pollution in space
01/02/2002EP1167978A1 Inertial sensor for suspension and control of an inertial reference in a satellite
01/02/2002EP1167820A2 Linear actuator especially for solar panel deployment systems for spacecraft
01/02/2002EP1167189A2 Correction of spacecraft steering control law for unexpected orbital inclination effects
01/02/2002EP1167188A1 Method for placing a payload into orbit by means of a hybrid multifunction booster rocket equipped with a liquid-fuel rocket propulsion system (lrps), hybrid multifunction booster rocket with cruising lrps and development test therefor
01/02/2002EP1165371A1 System and method for controlling the attitude of a spacecraft
01/02/2002EP1165370A2 Celestial object location device
01/02/2002EP0824451B1 Carbon fiber flocking for thermal management of compact missile electronics
01/01/2002US6336062 Attitude angle sensor correcting apparatus for an artificial satellite
01/01/2002US6334589 Cyanate ester composites for oxygen containment
12/2001
12/27/2001WO2001098143A1 Linear electromagnetic propelling device with open magnetic cores
12/27/2001US20010054503 Element with an electrically adjustable surface emissivity for infrared radiation
12/25/2001US6332592 Method for velocity precision pointing in spin-stabilized spacecraft or rockets
12/25/2001US6332591 Method of simulating external thermal fluxes absorbed by external radiating components of a spacecraft in flight, and spacecraft for implementing the method
12/25/2001US6332590 Photoemission based spacecraft charging sensor
12/20/2001DE10126797A1 Solare thermische Rakete Solar thermal rocket
12/19/2001EP1164078A2 Geostationary satellite station keeping method
12/19/2001EP1163152A2 Payload carry and launch system
12/18/2001US6331357 Articles with stable coatings having tailorable optical properties
12/18/2001US6330988 System for star catalog equalization to enhance attitude determination
12/18/2001US6330987 Apparatus and methods for in-space satellite operations
12/13/2001US20010051521 Elliptical satellite system which emulates the characteristics of geosynchronous satellites
12/13/2001US20010051218 Heat resistant coating a refractory metal silicide that is at least partially diffused into the base structure on at least one surface; for high temperature environments such as jets and rockets
12/13/2001US20010050657 Modular deployable antenna
12/12/2001EP1162598A2 Payload fairing with jettisonable mass acoustic suppression
12/12/2001EP1162139A1 Reusable booster for the first stage of a launcher
12/11/2001US6330093 Connector interface for spacecraft modules
12/11/2001US6328264 Artificial satellite with an orbit having a long staying time in a zenith direction, an orbit control method and a communication system therewith
12/06/2001US20010048051 Hypersonic and orbital vehicles system
12/05/2001EP1160876A2 Reconfigurable solar module array
12/05/2001EP1160542A2 Method for using satellite state vector prediction to provide satellite sensor automatic scan inhibit and/or sensor switching
12/04/2001US6327523 Overhead system of inclined eccentric geosynchronous orbitting satellites
12/04/2001US6325332 Coordinatable system of inclined geosynchronous satellite orbits
11/2001
11/29/2001WO2001091310A2 Multi-node point-to-point satellite communication system employing multiple geo satellites
11/29/2001WO2001089927A1 Method and device for integrating satellites on a launcher
11/29/2001WO2001089733A1 Aluminium alloy dome, in particular for forming a reservoir base, and method for making same
11/29/2001US20010045494 Method for limiting interference between satellite communications systems
11/29/2001DE10017699A1 Verglasung von Räumen, die einem extrem hohen Temperaturgradienten ausgesetzt sind Glazing of spaces which are exposed to an extremely high temperature gradient
11/29/2001DE10007372A1 Thermal protection system for space vehicles has generator in vehicle for generating electrodynamic field near part of outer vehicle surface exposed to heat
11/28/2001EP1157762A1 Dome made of aluminium alloy, especially to form a bottom of a tank and method to produce the same
11/28/2001EP1156960A1 Autonomous stratospheric airship
11/27/2001US6323817 Antenna cluster configuration for wide-angle coverage
11/27/2001US6322023 Evolvable propulsion module
11/27/2001US6321930 Cryogenic tank joint
11/27/2001US6321503 Foldable member
11/20/2001US6318676 Equatorial-normal body-stabilized spacecraft and control method for inclined orbit operation
11/20/2001US6318675 Solar wing thermal shock compensation using solar wing position actuator
11/20/2001US6318674 Power sphere deployment method
11/20/2001US6318673 Structure for the thermal insulation of satellites
11/20/2001US6318069 Ion thruster having grids made of oriented pyrolytic graphite
11/15/2001WO2001085542A1 Device and method for connecting two parts of a craft
11/15/2001WO2001056881A8 Virtually geostationary satellite array
11/15/2001US20010041950 Overhead system of inclined eccentric geosynchronous orbiting satellites
11/13/2001US6317661 Argument of perigee correction with longitude control for inclined, eccentric, geosynchronous satellites
11/13/2001US6317660 Method for using satellite state vector prediction to provide satellite sensor automatic scan inhibit and/or sensor switching
11/13/2001US6315248 Method for satellite injection using a solid fuel rocket motor
11/13/2001US6315247 Spacecraft with a microdynamic noise-free holding mechanism
11/13/2001US6314978 Reciprocating feed system for fluids
11/08/2001WO2001084666A2 Method for organizing a satellite communication service between subscribers
11/08/2001DE10107668A1 Solar heating rocket has solar concentrator which through selective directing devices focuses solar energy on heat storage section or on direct yield section
11/07/2001EP1152384A1 Flying object operating system
11/06/2001US6314344 Automated orbit compensation system and method
11/06/2001US6313811 Lightweight, compactly deployable support structure
11/06/2001US6312849 Method for producing a battery cell structure
11/06/2001US6311932 Yaw steering momentum system
11/06/2001US6311931 Bi-directional momentum bias spacecraft attitude control
11/06/2001US6311930 Anti-friction release device
11/06/2001US6311929 Spacecraft and appendage stepping methods that improve spacecraft attitude pointing and cancel solar array slew disturbances
11/06/2001US6311926 Space tram
11/06/2001US6311476 Integral propulsion and power radiant cavity receiver
11/01/2001WO2001081173A1 Louvers for spacecraft thermal control
11/01/2001US20010037248 Product warranty registration system and method
11/01/2001US20010037185 Method for determining the state variables of a moving rigid body in space
11/01/2001US20010035207 Space photovoltaic power generation system, power satellite, and control satellite
10/2001
10/31/2001EP1149765A2 Silicon thermal control blanket
10/31/2001EP1149764A2 Space photovoltaic power generation system, power satellite, and control satellite
10/31/2001EP1149763A2 Spacecraft having a dual reflector holddown for deploying multiple reflectors in a single release event
10/31/2001EP1148917A1 Mechanism for independently moving segments of a three-dimensional object and applications thereof
10/31/2001CN1320093A Holding and releasing mechanism with shape memory actuator
10/30/2001US6310336 Architecture for processing wide field-of view sun sensor signals for satellite applications
10/30/2001US6308919 Spacecraft having a dual reflector holddown for deploying multiple reflectors in a single release event
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