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CENTRE NAT DETUDES SPATIALES CNES

Overview
  • Total Patents
    29
  • GoodIP Patent Rank
    68,806
  • Filing trend
    ⇩ 100.0%
About

CENTRE NAT DETUDES SPATIALES CNES has a total of 29 patent applications. It decreased the IP activity by 100.0%. Its first patent ever was published in 2009. It filed its patents most often in France, EPO (European Patent Office) and Brazil. Its main competitors in its focus markets telecommunications, transport and measurement are SPACE SYSTEMS LORAL LLC, LORAL SPACE SYSTEMS INC and ALENIA SPAZIO SPA.

Patent filings in countries

World map showing CENTRE NAT DETUDES SPATIALES CNESs patent filings in countries

Patent filings per year

Chart showing CENTRE NAT DETUDES SPATIALES CNESs patent filings per year from 1900 to 2020

Top inventors

# Name Total Patents
#1 Capet Nicolas 3
#2 Peragin Eric 2
#3 Laurichesse Denis 2
#4 Rodriguez Urbano Jose 1
#5 Sauleau Ronan 1
#6 Perdu Philippe 1
#7 Masson Frederic 1
#8 Menudier Cyrille 1
#9 Boscaro Anthony 1
#10 Bibent Nicolas 1

Latest patents

Publication Filing date Title
FR3053166A1 Multi-beam source for multi-beam antenna
FR3051483A1 NOVEL SILICON ENRICHED COMPOSITE MATERIAL, METHOD FOR MANUFACTURING SAME, AND USE THEREOF AS ELECTRODE
FR3051612A1 Telecommunication method and system
FR3050982A1 Wheel desaturation driving unit, space engine attitude controlling device, and wheel desaturing method thereof
FR3049043A1 LIGHTING DEVICE FOR OBJECT ANALYSIS HAVING AT LEAST ONE REFLECTIVE AND / OR TRANSPARENT POLY SURFACE AND SYSTEM THEREFOR
FR3049145A1 OBJECT OBSERVATION BEACON, OBSERVATION SYSTEM AND METHOD FOR TRANSMITTING OBSERVATION DATA THEREOF
FR3047978A1 RESERVOIR OF A SPACE PROPULSION SYSTEM
FR3047859A1 ELECTROMAGNETIC WAVE EMISSION NETWORK ANTENNA CARRIER OF AN ORBITAL ANGULAR MOMENT AND TRANSMISSION METHOD THEREOF
FR3047329A1 METHOD AND DEVICE FOR RECONSTRUCTING A USEFUL SIGNAL FROM AN ACQUIRED NOISE SIGNAL
FR3046686A1 DEVICE FOR CONTROLLING THE ATTITUDE OF A SPACE DEVICE
FR3045957A1 ANTENNAIRE SYSTEM OF NETWORK TYPE
FR3033770A1 LAUNCHING AREA OF A PROPULSION AEROSPACE DEVICE BASED ON SOLID PROPERGOL AND METHOD OF PROTECTING SAME
FR3033056A1 METHOD FOR DETERMINING THE GUIDANCE PARAMETERS OF A SATELLITE FOR FOLLOWING A TRACK
FR3030455A1 INTER-ORBITAL TRANSFER METHOD
FR3023922A1 TRUST INDICATOR POSITIONING AND NAVIGATION RECEIVER
FR2999775A1 SUB-CRITICAL DUAL MASSES NUCLEAR REACTOR
FR2995448A1 OPTICAL DEVICE FOR EMISSION AND DETECTION OF LIGHT RAYS