Inventor profile of:

Jeremy C. Danforth

City:

Tucson, Arizona

Country:

United States

Published Applications:

26

Last publication date:

2021-04-15

Top Assignees for applications by Jeremy C. Danforth

The entities that hold a legal rights for patent applications filed by inventor Danforth Jeremy C.:

Recent patent applications by Danforth Jeremy C.

Jeremy C. Danforth from Tucson, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2021-04-15
US20210108598A1
Mechanical engineering

Hybrid rocket motor with integral oxidizer tank

#2 | 2020-01-23
US20200024210A1
Chemistry; metallurgy

Solid propellant additive manufacturing system

#3 | 2020-01-23
US20200024003A1
Performing operations; transporting

Satellite with integral thrusters

#4 | 2019-01-03
US20190002362A1
Chemistry; metallurgy

Additive manufactured combustible element with fuel and oxidizer

#5 | 2018-04-19
US20180106218A1
Mechanical engineering

Integrated thruster

#6 | 2018-03-15
US20180073842A1
Mechanical engineering

Projectile with single-piece main body

#7 | 2018-03-08
US20180069352A1
Electricity

Electrical device with shunt, and receptacle

#8 | 2018-03-08
US20180065202A1
Performing operations; transporting

Methods of making an electrical connection, and of making a receptacle for receiving an electrical device

#9 | 2018-02-22
US20180051657A1
Mechanical engineering

Microwave ignition of electrically operated propellants

#10 | 2018-02-15
US20180044257A1
Chemistry; metallurgy

Solid propellant additive manufacturing method and system

#11 | 2018-01-04
US20180003130A1
Mechanical engineering

Electrode ignition and control of electrically operated propellants

#12 | 2017-10-05
US20170284339A1
Mechanical engineering

THRUSTER WITH SEGMENTED PROPELLANT

#13 | 2017-10-05
US20170283095A1
Performing operations; transporting

Satellite with integral thrusters

#14 | 2017-09-07
US20170253537A1
Chemistry; metallurgy

Method of producing solid propellant element

#15 | 2017-09-07
US20170253536A1
Chemistry; metallurgy

Solid propellant with integral electrodes, and method

#16 | 2017-08-17
US20170234268A1
Mechanical engineering

Hybrid rocket motor with integral oxidizer tank

#17 | 2017-06-01
US20170153096A1
Mechanical engineering

Base drag reduction fairing using shape memory materials

#18 | 2017-05-18
US20170138310A1
Mechanical engineering

Aerospike rocket motor assembly

#19 | 2017-05-11
US20170131078A1
Mechanical engineering

Multifunctional aerodynamic, propulsion, and thermal control system

#20 | 2017-04-27
US20170113817A1
Performing operations; transporting

Spacecraft with shape memory polymer deployment mechanism

#21 | 2016-12-08
US20160356245A1
Mechanical engineering

ROCKET MOTOR PRODUCED BY ADDITIVE MANUFACTURING

#22 | 2016-12-08
US20160355447A1
Chemistry; metallurgy

Additive manufactured combustible element with fuel and oxidizer

#23 | 2014-05-22
US20140137539A1
Mechanical engineering

THRUST-PRODUCING DEVICE WITH DETONATION MOTOR

#24 | 2012-10-25
US20120269633A1
Mechanical engineering

Closed gas generator and micro power unit including the same

#25 | 2011-02-03
US20110023449A1
Mechanical engineering

Insensitive rocket motor

#26 | 2010-11-11
US20100282116A1
Mechanical engineering

Base drag reduction fairing

InventorID:

766311 ⎘