SNECMA PROPULSION SOLIDE
DEAD

Serial Number

78144972

Owner

SAFRAN

Attorney

Jeffrey H. Kaufman

Filing Date

Jul 17, 2002

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SNECMA PROPULSION SOLIDE Trademark

Serial Number: 78144972 • Registration: 3081540

SNECMA PROPULSION SOLIDE is a trademark filed by SAFRAN on July 17, 2002. The trademark is classified under Class 1 (Chemicals), Class 6 (Metal Goods), Class 7 (Machinery), Class 9 (Computers & Electronics), Class 11 (Environmental Control), Class 12 (Vehicles), Class 38 (Telecommunications), Class 40 (Treatment & Processing), Class 42 (Computer & Scientific), Class 13 (Firearms), Class 17 (Rubber Goods), Class 19 (Building Materials), Class 22 (Cordage). The application is currently no longer active.

Owner Contact Info

SAFRAN (73 trademarks)

2, BOULEVARD DE GENERAL MARTIAL VALIN
PARIS 75015 , FR

Entity Type: 03

Trademark Details

Filing Date

July 17, 2002

Registration Date

April 18, 2006

Published for Opposition

September 27, 2005

Cancellation Date

November 23, 2012

Goods & Services

Treatment of composite materials by siliconizing, carbonization, densification and physical-chemical treatments of fibers and textures; fabric finishing, fabric treatment, fiber, fabric and texture activation services; physical-chemical operations, namely, treatments of anti-oxidation and anti-corrosion protection of non-metallic composite materials

Electric, electronic and magnetic sensors for pressures, speeds, displacements, temperatures, positions, vibrations, constitutive parts of these sensors

Carbon fabrics for thermostructural composites, namely, rayon base fabrics; thermostructural composites for use in the field of aeronautics and space, nuclear research, heat treatment and the glass industry; refractory furnace lining, namely, soles, intermediate plates, spacers and lines made for industrial furnaces; refractory furnace linings, namely, thermal protections in the form of furnace coatings and layouts, with the exception of filters; structural parts for heat treatment furnaces, namely, plates and bridges, made up of non metallic composite materials

Solid propellant rocket engines for satellite launchers and for ballistic and tactical missiles and mechanical parts therefore

Stratified metals consisting of successive layers of elastomers and metallic or composite frameworks for use in the manufacture of satellites, rockets, missiles, aerospace vehicles, aircraft engines and brakes; metallic matrix composite materials (CMM) for use in the manufacture of satellites, rockets, missiles, aerospace vehicles, aircraft engines and brakes

Rings of rubber for use as pipe connection seals; non-metal pipe joints; non-metal fluid-type seals for hydraulic and fuel circuits used on aeronautical equipment; pipe gaskets; elastomeric plates; sealing packaging for couplings; stratified materials made of successive layers of elastomers and metallic or composite frameworks, plane, cylindrical, spherical, round or conical stratified products, namely, flexible rings, flexible seals, flexible bearings and stops, flexible articulated and non-articulated swivel joints, to ensure proper tightness between two or more rigid or flexible assemblies

Telecommunication services, namely, local and long distance transmission of voice, data, and graphics by means of telephone, telegraphic, cable, and satellite transmissions in the field of overhauling and standard replacement of engines and engine modules used in aeronautic and space applications; local and long distance transmission of voice, data and graphics by means of telephone, telegraphic, cable, and satellite transmissions concerning training for overhauling of engines and engine modules used in aeronautic and space applications; transmission of information by radio and television channels using or without using satellite communications, concerning overhauling, standard replacement, renting and training in the field of engines and engine modules used in aeronautic and space applications

Ballistic and tactical missiles propelled by rockets; electro-pyrotechnic initiators using a transmission of energy by laser beam, for pyrotechnical devices used on missiles; optopyrotechnical safety detonators

Thermostructural composite materials for use in satellites, rocks, missiles, aerospace vehicles, aircraft engines and brakes; synthetic and artificial resins for use in satellites, rockets, missiles, aerospace vehicles, aircraft engines and brakes; plastics in the form of powders, fluids and compounds, for use in the manufacture of satellites, rockets, missiles, aerospace vehicles, aircraft engines and brakes; chemical products for industrial applications, namely, chemicals for hardening and soldering metals, and for use in the manufacture of satellites, rockets, missiles, aerospace vehicles, aircraft engines and brakes; heat-resistant materials, namely, carbon-carbon, carbon-sic, and sic-sic composite materials for use in the manufacture of satellites, rockets, missiles, aerospace vehicles, aircraft engines and brakes; organic and ceramic matrix composite materials (CMO and CMC respectively) for use in the manufacture of satellites, rockets, missiles, aerospace vehicles, aircraft engines and brakes; absorbing carbons for use in the manufacture of satellites, rockets, missiles, aerospace vehicles, aircraft engines and brakes; chemical agents for textile material impregnation; non-metallic, heat resistant materials namely, carbon-carbon materials for use in propulsion, aeronautical brakes, equipment and tools for heat treating furnaces, and thermal protection equipment for nuclear applications; ceramic composites of the SIC/SIC and C/SIC type for use in propulsion and space

Aeronautic and astronautic vehicles, namely, space launchers, space vehicles, airplanes, helicopters; space rockets; space shuttles for use in space fitted with hypersonic propulsion systems; couplings and brakes for land vehicles, motor vehicles and railroad vehicles; brakes for air vehicles; and plastic honeycomb structures used as structural reinforcements in rockets, airplanes, and space vehicles

Heat and steam accumulators and regenerators; thermal exchangers for use in space propulsion applications; heat treatment furnaces and hearths; intermediate plates and spacers for use in furnaces, all made of composite materials with a carbon or ceramic perform, namely, reinforcement fiber texture; and heating resistors

Raw fibrous textile materials offering high mechanical and thermal or friction resistance and intended for engines, and more generally for aeronautical and aerospace applications, biomaterials, and friction parts such as brakes and clutches, namely, tri-dimensional interlock woven fabrics from carbon or ceramic untwisted stretch broken or continuous yarn, and textile architecture, reinforcement of composite materials, made by needle punching of multidirectional carbon fiber plies, obtained by plying of large ribbons of parallel discontinuous fibers or continuous fibers made of carbon, ceramic of carbon or ceramic precursors; and carbon fibers for textile use

Scientific and industrial research, namely, biological researches, chemical researches, morphological researches, thermal researches and mechanical engineering researches; research and development of new products for third parties; engineering work, namely, expert examinations and technical project studies; professional engineering consultancy services; testing of materials; laboratory services, namely, calibration and verification services in the sphere of metrology, chemistry, morphology and thermal engineering; preparation and design of software programs and computer programming for others

Filing History

CANCELLED SEC. 8 (6-YR)
Nov 23, 2012 C8..
AUTOMATIC UPDATE OF ASSIGNMENT OF OWNERSHIP
Sep 5, 2007 ASGN
REGISTERED-PRINCIPAL REGISTER
Apr 18, 2006 R.PR
1(B) BASIS DELETED; PROCEED TO REGISTRATION
Feb 28, 2006 DP1B
NOTICE OF ALLOWANCE CANCELLED
Feb 1, 2006 IUCN
TEAS DELETE 1(B) BASIS RECEIVED
Feb 1, 2006 D1BR
NOTICE OF ALLOWANCE CORRECTION ENTERED
Jan 21, 2006 ICNA
FAX RECEIVED
Jan 18, 2006 FAXX
NOA MAILED - SOU REQUIRED FROM APPLICANT
Dec 20, 2005 NOAM
PUBLISHED FOR OPPOSITION
Sep 27, 2005 PUBO
NOTICE OF PUBLICATION
Sep 7, 2005 NPUB
LAW OFFICE PUBLICATION REVIEW COMPLETED
Jun 13, 2005 PREV
ASSIGNED TO LIE
Jun 10, 2005 ALIE
APPROVED FOR PUB - PRINCIPAL REGISTER
Jun 3, 2005 CNSA
AMENDMENT FROM APPLICANT ENTERED
May 5, 2005 ACEC
CORRESPONDENCE RECEIVED IN LAW OFFICE
May 2, 2005 CRFA
PAPER RECEIVED
May 2, 2005 MAIL
NON-FINAL ACTION E-MAILED
Nov 1, 2004 GNRT
NON-FINAL ACTION WRITTEN
Nov 1, 2004 CNRT
PREVIOUS ALLOWANCE COUNT WITHDRAWN
Oct 21, 2004 ZZZX
LAW OFFICE PUBLICATION REVIEW COMPLETED
Aug 18, 2004 PREV
ASSIGNED TO LIE
Aug 13, 2004 ALIE
APPROVED FOR PUB - PRINCIPAL REGISTER
Aug 7, 2004 CNSA
AMENDMENT FROM APPLICANT ENTERED
Jul 16, 2004 ACEC
CORRESPONDENCE RECEIVED IN LAW OFFICE
Jul 16, 2004 CRFA
PAPER RECEIVED
Jul 16, 2004 MAIL
NON-FINAL ACTION E-MAILED
Jan 20, 2004 GNRT
PREVIOUS ALLOWANCE COUNT WITHDRAWN
Jan 7, 2004 ZZZX
APPROVED FOR PUB - PRINCIPAL REGISTER
Nov 2, 2003 CNSA
CORRESPONDENCE RECEIVED IN LAW OFFICE
Sep 23, 2003 CRFA
PAPER RECEIVED
Sep 23, 2003 MAIL
LETTER OF SUSPENSION E-MAILED
Jul 25, 2003 GNSL
CASE FILE IN TICRS
Jun 18, 2003 CFIT
CORRESPONDENCE RECEIVED IN LAW OFFICE
May 27, 2003 CRFA
PAPER RECEIVED
May 27, 2003 MAIL
PAPER RECEIVED
Nov 29, 2002 MAIL
NON-FINAL ACTION E-MAILED
Nov 24, 2002 GNRT
ASSIGNED TO EXAMINER
Nov 18, 2002 DOCK
PAPER RECEIVED
Aug 15, 2002 MAIL