Matt H. Summers

Person

Marana, AZ, US

People

Patents Grantslast 30 patents

Information Patent Grant
Lightweight thermal battery system for high-temperature environments
- Patent number 11,335,917
- Issue date May 17, 2022
- Raytheon Company
- Dean Dickherber
- H01 - BASIC ELECTRIC ELEMENTS
Information Patent Grant
Hybrid rocket motor with integral oxidizer tank
- Patent number 11,326,556
- Issue date May 10, 2022
- Raytheon Company
- Matt H. Summers
- B33 - ADDITIVE MANUFACTURING TECHNOLOGY
Information Patent Grant
Solid propellant additive manufacturing system
- Patent number 11,208,362
- Issue date Dec 28, 2021
- Raytheon Company
- Matthew H. Summers
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Satellite with integral thrusters
- Patent number 11,174,048
- Issue date Nov 16, 2021
- Raytheon Company
- Frederick B. Koehler
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Resin transfer molded rocket motor nozzle with adaptive geometry
- Patent number 11,028,803
- Issue date Jun 8, 2021
- Raytheon Company
- Matt H. Summers
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Hybrid rocket motor with integral oxidizer tank
- Patent number 10,823,115
- Issue date Nov 3, 2020
- Raytheon Company
- Matt H. Summers
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Microwave ignition of electrically operated propellants
- Patent number 10,808,649
- Issue date Oct 20, 2020
- Raytheon Company
- James K. Villarreal
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Rocket motor with combustion product deflector
- Patent number 10,690,443
- Issue date Jun 23, 2020
- Raytheon Company
- Matt H. Summers
- F42 - AMMUNITION BLASTING
Information Patent Grant
Integrated thruster
- Patent number 10,662,898
- Issue date May 26, 2020
- Raytheon Company
- Matthew H. Summers
- F42 - AMMUNITION BLASTING
Information Patent Grant
Additive manufactured combustible element with fuel and oxidizer
- Patent number 10,654,762
- Issue date May 19, 2020
- Raytheon Company
- Jeremy C. Danforth
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Electrical device with shunt, and receptacle
- Patent number 10,615,547
- Issue date Apr 7, 2020
- Raytheon Company
- Matthew H. Summers
- F42 - AMMUNITION BLASTING
Information Patent Grant
Electrically operated propellant for solid rocket motor thrust mana...
- Patent number 10,563,617
- Issue date Feb 18, 2020
- Raytheon Company
- James K. Villarreal
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Spacecraft with shape memory polymer deployment mechanism
- Patent number 10,518,908
- Issue date Dec 31, 2019
- Raytheon Company
- Frederick B. Koehler
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Solid propellant additive manufacturing method and system
- Patent number 10,287,218
- Issue date May 14, 2019
- Raytheon Company
- Matthew H. Summers
- C06 - EXPLOSIVES MATCHES
Information Patent Grant
Solid propellant with integral electrodes, and method
- Patent number 10,259,756
- Issue date Apr 16, 2019
- Raytheon Company
- Jeremy C. Danforth
- B05 - SPRAYING OR ATOMISING IN GENERAL APPLYING LIQUIDS OR OTHER FLUENT MATER...
Information Patent Grant
Projectile with single-piece main body
- Patent number 10,247,530
- Issue date Apr 2, 2019
- Raytheon Company
- Jeremy C. Danforth
- F42 - AMMUNITION BLASTING
Information Patent Grant
Satellite with integral thrusters
- Patent number 10,220,966
- Issue date Mar 5, 2019
- Raytheon Company
- Frederick B. Koehler
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Grant
Base drag reduction fairing using shape memory materials
- Patent number 10,184,762
- Issue date Jan 22, 2019
- Raytheon Company
- Matthew H. Summers
- F42 - AMMUNITION BLASTING
Information Patent Grant
Electrode ignition and control of electrically operated propellants
- Patent number 10,145,337
- Issue date Dec 4, 2018
- Raytheon Company
- Matt H. Summers
- B60 - VEHICLES IN GENERAL
Information Patent Grant
Electrically operated pulse initiators and ignition
- Patent number 10,107,601
- Issue date Oct 23, 2018
- Raytheon Company
- James Kendall Villarreal
- F42 - AMMUNITION BLASTING
Information Patent Grant
Additive manufactured combustible element with fuel and oxidizer
- Patent number 10,093,592
- Issue date Oct 9, 2018
- Raytheon Company
- Jeremy C. Danforth
- B33 - ADDITIVE MANUFACTURING TECHNOLOGY
Information Patent Grant
Methods of making an electrical connection, and of making a recepta...
- Patent number 10,046,409
- Issue date Aug 14, 2018
- Raytheon Company
- Matthew H. Summers
- B23 - MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR
Information Patent Grant
Method of producing solid propellant element
- Patent number 10,023,505
- Issue date Jul 17, 2018
- Raytheon Company
- Jeremy C. Danforth
- B29 - WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
Information Patent Grant
Multifunctional aerodynamic, propulsion, and thermal control system
- Patent number 10,018,456
- Issue date Jul 10, 2018
- Raytheon Company
- Paul M. Lyons
- F42 - AMMUNITION BLASTING
Information Patent Grant
Electrically controlled variable force deployment airbag and inflation
- Patent number 9,457,761
- Issue date Oct 4, 2016
- Raytheon Company
- James K. Villarreal
- B60 - VEHICLES IN GENERAL

Patents Applicationslast 30 patents

Information Patent Application
HYBRID ROCKET MOTOR WITH INTEGRAL OXIDIZER TANK
- Publication number 20210108598
- Publication date Apr 15, 2021
- Raytheon Company
- Matt H. Summers
- B33 - ADDITIVE MANUFACTURING TECHNOLOGY
Information Patent Application
ROCKET MOTOR WITH COMBUSTION PRODUCT DEFLECTOR
- Publication number 20200225002
- Publication date Jul 16, 2020
- Raytheon Company
- Matt H. Summers
- F42 - AMMUNITION BLASTING
Information Patent Application
LIGHTWEIGHT THERMAL BATTERY SYSTEM FOR HIGH-TEMPERATURE ENVIRONMENTS
- Publication number 20200144631
- Publication date May 7, 2020
- Raytheon Company
- Dean Dickherber
- H01 - BASIC ELECTRIC ELEMENTS
Information Patent Application
RESIN TRANSFER MOLDED ROCKET MOTOR NOZZLE WITH ADAPTIVE GEOMETRY
- Publication number 20200080518
- Publication date Mar 12, 2020
- Raytheon Company
- Matt H. Summers
- B29 - WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
Information Patent Application
SOLID PROPELLANT ADDITIVE MANUFACTURING SYSTEM
- Publication number 20200024210
- Publication date Jan 23, 2020
- Raytheon Company
- Matthew H. Summers
- C06 - EXPLOSIVES MATCHES
Information Patent Application
SATELLITE WITH INTEGRAL THRUSTERS
- Publication number 20200024003
- Publication date Jan 23, 2020
- Frederick B. Koehler
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ADDITIVE MANUFACTURED COMBUSTIBLE ELEMENT WITH FUEL AND OXIDIZER
- Publication number 20190002362
- Publication date Jan 3, 2019
- Raytheon Company
- Jeremy C. Danforth
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ELECTRICALLY OPERATED PROPELLANT THRUST ASSIST FOR SUPPLEMENTING AI...
- Publication number 20180273193
- Publication date Sep 27, 2018
- Raytheon Company
- Matt H. Summers
- C06 - EXPLOSIVES MATCHES
Information Patent Application
ELECTRICALLY OPERATED PROPELLANT FOR SOLID ROCKET MOTOR THRUST MANA...
- Publication number 20180128207
- Publication date May 10, 2018
- Raytheon Company
- James K. Villarreal
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
INTEGRATED THRUSTER
- Publication number 20180106218
- Publication date Apr 19, 2018
- Raytheon Company
- Matthew H. Summers
- F42 - AMMUNITION BLASTING
Information Patent Application
PROJECTILE WITH SINGLE-PIECE MAIN BODY
- Publication number 20180073842
- Publication date Mar 15, 2018
- Raytheon Company
- Jeremy C. Danforth
- B33 - ADDITIVE MANUFACTURING TECHNOLOGY
Information Patent Application
ELECTRICAL DEVICE WITH SHUNT, AND RECEPTACLE
- Publication number 20180069352
- Publication date Mar 8, 2018
- Raytheon Company
- Matthew H. Summers
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
METHODS OF MAKING AN ELECTRICAL CONNECTION, AND OF MAKING A RECEPTA...
- Publication number 20180065202
- Publication date Mar 8, 2018
- Raytheon Company
- Matthew H. Summers
- B33 - ADDITIVE MANUFACTURING TECHNOLOGY
Information Patent Application
ACTUATOR STRUCTURE AND METHOD OF IGNITION OF ELECTRICALLY OPERATED...
- Publication number 20180058377
- Publication date Mar 1, 2018
- Raytheon Company
- James K. Villarreal
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
MICROWAVE IGNITION OF ELECTRICALLY OPERATED PROPELLANTS
- Publication number 20180051657
- Publication date Feb 22, 2018
- Raytheon Company
- James K. Villarreal
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ELECTRODE IGNITION AND CONTROL OF ELECTRICALLY OPERATED PROPELLANTS
- Publication number 20180003130
- Publication date Jan 4, 2018
- Raytheon Company
- Matt H. Summers
- B60 - VEHICLES IN GENERAL
Information Patent Application
SATELLITE WITH INTEGRAL THRUSTERS
- Publication number 20170283095
- Publication date Oct 5, 2017
- Frederick B. Koehler
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
THRUSTER WITH SEGMENTED PROPELLANT
- Publication number 20170284339
- Publication date Oct 5, 2017
- Frederick B. Koehler
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
METHOD OF PRODUCING SOLID PROPELLANT ELEMENT
- Publication number 20170253537
- Publication date Sep 7, 2017
- Raytheon Company
- Jeremy C. Danforth
- B33 - ADDITIVE MANUFACTURING TECHNOLOGY
Information Patent Application
SOLID PROPELLANT WITH INTEGRAL ELECTRODES, AND METHOD
- Publication number 20170253536
- Publication date Sep 7, 2017
- Raytheon Company
- Jeremy C. Danforth
- B05 - SPRAYING OR ATOMISING IN GENERAL APPLYING LIQUIDS OR OTHER FLUENT MATER...
Information Patent Application
HYBRID ROCKET MOTOR WITH INTEGRAL OXIDIZER TANK
- Publication number 20170234268
- Publication date Aug 17, 2017
- Raytheon Company
- Matt H. Summers
- B33 - ADDITIVE MANUFACTURING TECHNOLOGY
Information Patent Application
BASE DRAG REDUCTION FAIRING USING SHAPE MEMORY MATERIALS
- Publication number 20170153096
- Publication date Jun 1, 2017
- Raytheon Company
- Matthew H. Summers
- F42 - AMMUNITION BLASTING
Information Patent Application
MULTIFUNCTIONAL AERODYNAMIC, PROPULSION, AND THERMAL CONTROL SYSTEM
- Publication number 20170131078
- Publication date May 11, 2017
- Raytheon Company
- Paul M. Lyons
- F42 - AMMUNITION BLASTING
Information Patent Application
SPACECRAFT WITH SHAPE MEMORY POLYMER DEPLOYMENT MECHANISM
- Publication number 20170113817
- Publication date Apr 27, 2017
- Raytheon Company
- Frederick B. Koehler
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ELECTRICALLY OPERATED PULSE INITIATORS AND IGNITION
- Publication number 20170097213
- Publication date Apr 6, 2017
- Raytheon Company
- James Kendall Villarreal
- F42 - AMMUNITION BLASTING
Information Patent Application
ADDITIVE MANUFACTURED COMBUSTIBLE ELEMENT WITH FUEL AND OXIDIZER
- Publication number 20160355447
- Publication date Dec 8, 2016
- Raytheon Company
- Jeremy C. Danforth
- B33 - ADDITIVE MANUFACTURING TECHNOLOGY
Information Patent Application
ROCKET MOTOR PRODUCED BY ADDITIVE MANUFACTURING
- Publication number 20160356245
- Publication date Dec 8, 2016
- Raytheon Company
- Jeremy C. Danforth
- F02 - COMBUSTION ENGINES HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
Information Patent Application
ELECTRICALLY CONTROLLED VARIABLE FORCE DEPLOYMENT AIRBAG AND INFLATION
- Publication number 20150343988
- Publication date Dec 3, 2015
- Raytheon Company
- James K. Villarreal
- B60 - VEHICLES IN GENERAL

Matt H. Summers

Person

Patents Grantslast 30 patents

Lightweight thermal battery system for high-temperature environments

Hybrid rocket motor with integral oxidizer tank

Solid propellant additive manufacturing system

Satellite with integral thrusters

Resin transfer molded rocket motor nozzle with adaptive geometry

Hybrid rocket motor with integral oxidizer tank

Microwave ignition of electrically operated propellants

Rocket motor with combustion product deflector

Integrated thruster

Additive manufactured combustible element with fuel and oxidizer

Electrical device with shunt, and receptacle

Electrically operated propellant for solid rocket motor thrust mana...

Spacecraft with shape memory polymer deployment mechanism

Solid propellant additive manufacturing method and system

Solid propellant with integral electrodes, and method

Projectile with single-piece main body

Satellite with integral thrusters

Base drag reduction fairing using shape memory materials

Electrode ignition and control of electrically operated propellants

Electrically operated pulse initiators and ignition

Additive manufactured combustible element with fuel and oxidizer

Methods of making an electrical connection, and of making a recepta...

Method of producing solid propellant element

Multifunctional aerodynamic, propulsion, and thermal control system

Electrically controlled variable force deployment airbag and inflation

Patents Applicationslast 30 patents

HYBRID ROCKET MOTOR WITH INTEGRAL OXIDIZER TANK

ROCKET MOTOR WITH COMBUSTION PRODUCT DEFLECTOR

LIGHTWEIGHT THERMAL BATTERY SYSTEM FOR HIGH-TEMPERATURE ENVIRONMENTS

RESIN TRANSFER MOLDED ROCKET MOTOR NOZZLE WITH ADAPTIVE GEOMETRY

SOLID PROPELLANT ADDITIVE MANUFACTURING SYSTEM

SATELLITE WITH INTEGRAL THRUSTERS

ADDITIVE MANUFACTURED COMBUSTIBLE ELEMENT WITH FUEL AND OXIDIZER

ELECTRICALLY OPERATED PROPELLANT THRUST ASSIST FOR SUPPLEMENTING AI...

ELECTRICALLY OPERATED PROPELLANT FOR SOLID ROCKET MOTOR THRUST MANA...

INTEGRATED THRUSTER

PROJECTILE WITH SINGLE-PIECE MAIN BODY

ELECTRICAL DEVICE WITH SHUNT, AND RECEPTACLE

METHODS OF MAKING AN ELECTRICAL CONNECTION, AND OF MAKING A RECEPTA...

ACTUATOR STRUCTURE AND METHOD OF IGNITION OF ELECTRICALLY OPERATED...

MICROWAVE IGNITION OF ELECTRICALLY OPERATED PROPELLANTS

ELECTRODE IGNITION AND CONTROL OF ELECTRICALLY OPERATED PROPELLANTS

SATELLITE WITH INTEGRAL THRUSTERS

THRUSTER WITH SEGMENTED PROPELLANT

METHOD OF PRODUCING SOLID PROPELLANT ELEMENT

SOLID PROPELLANT WITH INTEGRAL ELECTRODES, AND METHOD

HYBRID ROCKET MOTOR WITH INTEGRAL OXIDIZER TANK

BASE DRAG REDUCTION FAIRING USING SHAPE MEMORY MATERIALS

MULTIFUNCTIONAL AERODYNAMIC, PROPULSION, AND THERMAL CONTROL SYSTEM

SPACECRAFT WITH SHAPE MEMORY POLYMER DEPLOYMENT MECHANISM

ELECTRICALLY OPERATED PULSE INITIATORS AND IGNITION

ADDITIVE MANUFACTURED COMBUSTIBLE ELEMENT WITH FUEL AND OXIDIZER

ROCKET MOTOR PRODUCED BY ADDITIVE MANUFACTURING

ELECTRICALLY CONTROLLED VARIABLE FORCE DEPLOYMENT AIRBAG AND INFLATION