Daniel Chasman

Person

Tucson, AZ, US

People

Patents Grantslast 30 patents

Information Patent Grant
Integral injection thrust vector control with booster attitude cont...
- Patent number 9,115,964
- Issue date Aug 25, 2015
- Raytheon Company
- Andrew B Facciano
- F42 - AMMUNITION BLASTING
Information Patent Grant
Slotted multi-nozzle grid with integrated cooling channels
- Patent number 9,115,666
- Issue date Aug 25, 2015
- Raytheon Company
- Daniel Chasman
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Rocket multi-nozzle grid assembly and methods for maintaining press...
- Patent number 8,596,040
- Issue date Dec 3, 2013
- Raytheon Company
- Daniel Chasman
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Hybrid missile propulsion system with reconfigurable multinozzle grid
- Patent number 8,117,847
- Issue date Feb 21, 2012
- Raytheon Company
- Stephen D. Haight
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Propulsion system with canted multinozzle grid
- Patent number 7,856,806
- Issue date Dec 28, 2010
- Raytheon Company
- Daniel Chasman
- F42 - AMMUNITION BLASTING
Information Patent Grant
Missile control system and method
- Patent number 7,287,725
- Issue date Oct 30, 2007
- Raytheon Company
- Daniel B. Chasman
- F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF...
Information Patent Grant
Missile control system and method
- Patent number 7,108,223
- Issue date Sep 19, 2006
- Raytheon Company
- Daniel Chasman
- F42 - AMMUNITION BLASTING

Patents Applicationslast 30 patents

Information Patent Application
INTEGRAL INJECTION THRUST VECTOR CONTROL WITH BOOSTER ATTITUDE CONT...
- Publication number 20150184988
- Publication date Jul 2, 2015
- Raytheon Company
- Andrew B Facciano
- F42 - AMMUNITION BLASTING
Information Patent Application
SLOTTED MULTI-NOZZLE GRID WITH INTEGRATED COOLING CHANNELS
- Publication number 20140096510
- Publication date Apr 10, 2014
- Raytheon Company
- Daniel Chasman
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ROCKET MULTI-NOZZLE GRID ASSEMBLY AND METHODS FOR MAINTAINING PRESS...
- Publication number 20120233979
- Publication date Sep 20, 2012
- Raytheon Company
- Daniel Chasman
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
PROPULSION SYSTEM WITH CANTED MULTINOZZLE GRID
- Publication number 20100313544
- Publication date Dec 16, 2010
- Daniel Chasman
- F42 - AMMUNITION BLASTING
Information Patent Application
HYBRID MISSILE PROPULSION SYSTEM WITH RECONFIGURABLE MULTINOZZLE GRID
- Publication number 20090229241
- Publication date Sep 17, 2009
- Stephen D. Haight
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
MISSILE CONTROL SYSTEM AND METHOD
- Publication number 20060284006
- Publication date Dec 21, 2006
- Daniel B. Chasman
- F42 - AMMUNITION BLASTING
Information Patent Application
MISSILE CONTROL SYSTEM AND METHOD
- Publication number 20050011989
- Publication date Jan 20, 2005
- Daniel Chasman
- F42 - AMMUNITION BLASTING
Information Patent Application
Multi-nozzle grid missile propulsion system
- Publication number 20040084566
- Publication date May 6, 2004
- Daniel Chasman
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS

Daniel Chasman

Person

Patents Grantslast 30 patents

Integral injection thrust vector control with booster attitude cont...

Slotted multi-nozzle grid with integrated cooling channels

Rocket multi-nozzle grid assembly and methods for maintaining press...

Hybrid missile propulsion system with reconfigurable multinozzle grid

Propulsion system with canted multinozzle grid

Missile control system and method

Missile control system and method

Patents Applicationslast 30 patents

INTEGRAL INJECTION THRUST VECTOR CONTROL WITH BOOSTER ATTITUDE CONT...

SLOTTED MULTI-NOZZLE GRID WITH INTEGRATED COOLING CHANNELS

ROCKET MULTI-NOZZLE GRID ASSEMBLY AND METHODS FOR MAINTAINING PRESS...

PROPULSION SYSTEM WITH CANTED MULTINOZZLE GRID

HYBRID MISSILE PROPULSION SYSTEM WITH RECONFIGURABLE MULTINOZZLE GRID

MISSILE CONTROL SYSTEM AND METHOD

MISSILE CONTROL SYSTEM AND METHOD

Multi-nozzle grid missile propulsion system