Inventor profile of:

Mark T. Langhenry

City:

Tucson, Arizona

Country:

United States

Published Applications:

19

Last publication date:

2022-06-02

Top Assignees for applications by Mark T. Langhenry

The entities that hold a legal rights for patent applications filed by inventor Langhenry Mark T.:

Recent patent applications by Langhenry Mark T.

Mark T. Langhenry from Tucson, US has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2022-06-02
US20220170432A1
Mechanical engineering

Multi-pulse solid rocket motor ignition method

#2 | 2021-03-04
US20210062764A1
Mechanical engineering

EFFECTOR HEALTH MONITOR SYSTEM AND METHODS FOR SAME

#3 | 2020-03-12
US20200080518A1
Mechanical engineering

Resin transfer molded rocket motor nozzle with adaptive geometry

#4 | 2020-01-23
US20200024210A1
Chemistry; metallurgy

Solid propellant additive manufacturing system

#5 | 2020-01-23
US20200024003A1
Performing operations; transporting

Satellite with integral thrusters

#6 | 2019-01-03
US20190002362A1
Chemistry; metallurgy

Additive manufactured combustible element with fuel and oxidizer

#7 | 2018-09-27
US20180273193A1
Performing operations; transporting

ELECTRICALLY OPERATED PROPELLANT THRUST ASSIST FOR SUPPLEMENTING AIRPLANE TAKEOFF, LANDING OR IN-FLIGHT MANEUVERABILITY

#8 | 2018-05-10
US20180128207A1
Mechanical engineering

Electrically operated propellant for solid rocket motor thrust management

#9 | 2018-03-01
US20180058377A1
Mechanical engineering

ACTUATOR STRUCTURE AND METHOD OF IGNITION OF ELECTRICALLY OPERATED PROPELLANT

#10 | 2018-02-22
US20180051657A1
Mechanical engineering

Microwave ignition of electrically operated propellants

#11 | 2018-02-15
US20180044257A1
Chemistry; metallurgy

Solid propellant additive manufacturing method and system

#12 | 2018-01-04
US20180003130A1
Mechanical engineering

Electrode ignition and control of electrically operated propellants

#13 | 2017-10-05
US20170284339A1
Mechanical engineering

THRUSTER WITH SEGMENTED PROPELLANT

#14 | 2017-10-05
US20170283095A1
Performing operations; transporting

Satellite with integral thrusters

#15 | 2017-05-18
US20170138310A1
Mechanical engineering

Aerospike rocket motor assembly

#16 | 2017-04-06
US20170097213A1
Mechanical engineering

Electrically operated pulse initiators and ignition

#17 | 2016-12-08
US20160356245A1
Mechanical engineering

ROCKET MOTOR PRODUCED BY ADDITIVE MANUFACTURING

#18 | 2016-12-08
US20160355447A1
Chemistry; metallurgy

Additive manufactured combustible element with fuel and oxidizer

#19 | 2015-12-03
US20150343988A1
Performing operations; transporting

Electrically controlled variable force deployment airbag and inflation

InventorID:

1374585 ⎘