We have observed
19 EP applications
has served for within the last five+ years.
(We consider all applications which have an EP A1 or A2 publication dated after September 19, 2014).
Please note, that we only count EP applications,
in which the name of the patent attorney is explicitly mentioned as representative.
These EP applications are:
TWO-DIMENSIONAL MULTI-BEAM FORMER, ANTENNA COMPRISING SUCH A MULTI-BEAM FORMER AND SATELLITE TELECOMMUNICATION SYSTEM COMPRISING SUCH AN ANTENNA
Method for producing an antenna reflector with formed surface, reflector with formed surface obtained by said method and antenna comprising such a reflector
Power divider including a T-coupler in the E-plane, radiating network and antenna including such a radiating network
Bi-polarisation compact power distributor, network of a plurality of distributors, compact radiating element and planar antenna having such a distributor
SATELLITE TRANSMISSION AND RECEPTION DEVICE WITH HIGH MULTIPATH ATTENUATION, REPEATER AND SATELLITE PROVIDED WITH SUCH A DEVICE
Satellite communication system for continuous broadband access service over a land covered area including at least one polar region with a constellation of satellites on circular orbit at a low or medium altitude.
Radio-frequency method and system for determining, using spacecraft torque, the relative angular position between a plurality of remote spacecraft
ASSEMBLY OF TWO DUAL-REFLECTOR ANTENNAS MOUNTED ON A COMMON MOUNTING AND A SATELLITE COMPRISING SAID ASSEMBLY
METHOD FOR DIGITALLY COMPENSATING VARIATIONS, BASED ON THE TEMPERATURE, OF AN ELECTRICAL VARIABLE OF AN ONBOARD SPATIAL RADIO FREQUENCY TELECOMMUNICATIONS DEVICE
ANTENNA WITH SHAPED REFLECTOR(S) RECONFIGURABLE IN ORBIT
COMPACT BUTLER MATRIX , PLANAR BI-DIMENSIONAL BEAM-FORMER, AND PLANAR ANTENNA WITH SUCH A BUTLER MATRIX
SYSTEM FOR CONTROLLING A PLURALITY OF ELECTRICAL THRUSTERS FOR A SATELLITE AND ELECTRIC PROPULSION DEVICE COMPRISING SUCH A CONTROL SYSTEM
QUASI-OPTICAL LENS BEAM FORMER AND PLANAR ANTENNA COMPRISING SUCH A BEAM FORMER
FLEXIBLE SOLAR GENERATOR PROVIDED WITH ELECTRICAL PROTECTION AGAINST IMPACTS OF CELESTIAL OBJECTS, SPACECRAFT AND SATELLITE COMPRISING AT LEAST ONE SUCH SOLAR GENERATOR
COMPACT MULTI-FREQUENCY FEED HORN, RADIATING SOURCE AND ANTENNA COMPRISING SUCH A FEED HORN
HYBRID OPTICAL SYSTEM WITH REDUCED SIZE FOR IMAGING ARRAY ANTENNA
COMPACT BIPOLARISATION DRIVE ASSEMBLY FOR A RADIATING ANTENNA ELEMENT AND COMPACT NETWORK COMPRISING AT LEAST FOUR COMPACT DRIVE ASSEMBLIES
ACTIVE ANTENNA ARCHITECTURE WITH RECONFIGURABLE HYBRID BEAM FORMATION
DEPLOYABLE STRUCTURE COMPRISING A SET OF SOLAR GENERATORS, SYSTEM FOR DEPLOYING SUCH A DEPLOYABLE STRUCTURE AND SATELLITE COMPRISING SUCH A SYSTEM