Search

Jason D Flathom

from Irvine, CA
Age ~50
Get Report
Also known as:
Lathon F Jason, Lathorn F Jason
Phone and address:
12 Ticonderoga, Irvine, CA 92620
(949) 651-6187
Related to:
Beverly J Bohannon, 99Joey Scardina, 63Antonina Scardina, 93Jeffrey Bohannon, 38John Scardina, 65Jill A, 55
Connected to:
Teri S Flati, 66Ashley Flatland, 47Lori A Flatland, 54Richmond Flatland, 100Anne W Flatley, 49Brittanee D Flatley, 36Carol A Flatley, 56Chris Flatley, 50Erin E Flatley, 40James Flatley, 65

Jason Flathom Phones & Addresses

  • 12 Ticonderoga, Irvine, CA 92620 (949) 651-6187
  • 19 Milazzo, Irvine, CA 92620 (714) 730-9779
  • San Jose, CA
  • Oak Lawn, IL
  • Milwaukee, WI
  • Orange, CA
  • 19 Milazzo, Irvine, CA 92620 (949) 637-3966

Work

Company: Boeing Jul 2017 Position: Space vehicle design ipt lead

Education

Degree: Bachelors, Bachelor of Science School / High School: Marquette University 1993 to 1997 Specialities: Mechanical Engineering

Skills

Aerospace • Engineering • Mechanical Engineering • Manufacturing • Catia • Product Development • Solidworks • Lean Manufacturing • Mechanical Systems • Engineering Management • Systems Design • Integration • Aircraft • Mechanical Product Design • Composites • Structural Engineering • Testing • Manufacturing Engineering • Project Management • Project Planning • Project Engineering • Project Coordination • Ptc Creo • Competitive Analysis • Systems Engineering • Earned Value Management • Root Cause Analysis • Opto Mechanical Design • Opto Mechanical Engineering • Space Systems • Spacecraft • Satellite • Requirements Management • Cross Functional Team Leadership • Program Management • Microsoft Office • Configuration Management • Cost Accounting • Cost Management • Vendor Management • Team Leadership • Team Management • Cross Functional Collaborations • Computer Aided Design • Design Research • Mechanical Testing • Composite Structures • Aerospace Engineering • Functional Requirements

Emails

j***[email protected]

Industries

Aviation & Aerospace

Resumes

Resumes

Jason Flathom Photo 1

Space Vehicle Design Ipt Lead

View page
Location:
Sugar City, ID
Industry:
Aviation & Aerospace
Work:
Boeing
Space Vehicle Design Ipt Lead
Boeing Jul 2011 - Jul 2017
Lead Mechanical Space Vehicle Engineer
Boeing Jul 2009 - Jul 2011
Senior Mechanical Designer
Northrop Grumman Corporation Aug 2008 - Feb 2009
Structures Engineer
Boeing Jun 2006 - Jun 2008
Structural Engineer
Education:
Marquette University 1993 - 1997
Bachelors, Bachelor of Science, Mechanical Engineering
Skills:
Aerospace
Engineering
Mechanical Engineering
Manufacturing
Catia
Product Development
Solidworks
Lean Manufacturing
Mechanical Systems
Engineering Management
Systems Design
Integration
Aircraft
Mechanical Product Design
Composites
Structural Engineering
Testing
Manufacturing Engineering
Project Management
Project Planning
Project Engineering
Project Coordination
Ptc Creo
Competitive Analysis
Systems Engineering
Earned Value Management
Root Cause Analysis
Opto Mechanical Design
Opto Mechanical Engineering
Space Systems
Spacecraft
Satellite
Requirements Management
Cross Functional Team Leadership
Program Management
Microsoft Office
Configuration Management
Cost Accounting
Cost Management
Vendor Management
Team Leadership
Team Management
Cross Functional Collaborations
Computer Aided Design
Design Research
Mechanical Testing
Composite Structures
Aerospace Engineering
Functional Requirements

Publications

Us Patents

Precision Mirror Displacement Assembly

View page
US Patent:
20050046979, Mar 3, 2005
Filed:
Jun 21, 2004
Appl. No.:
10/872980
Inventors:
Dave Hiley - Los Angeles CA, US
Jason Flathom - Irvine CA, US
Tal Kiani - Redondo Beach CA, US
Mario Palombo - Manhattan Beach CA, US
Jose Bernal - Lomita CA, US
International Classification:
G02B026/08
G02B007/182
US Classification:
359877000
Abstract:
A precision mirror displacement assembly for controlling rotation of a mirror about a rotational axis to obtain a precise mirror orientation includes a mirror having an enhanced backside and a reflective front surface. The enhanced backside has a sufficient thickness to provide that attachment of mirror displacement control components, such as portions of actuator and position sensor assemblies, to the backside during manufacture of the mirror assembly does not cause distortion of the reflective front surface of the mirror. The enhanced backside also is of sufficient thickness to avoid distortion of the front surface based on interaction of the mirror with mechanical stops and actuator components that are attached to a base of a separate housing of the mirror assembly that opposes the backside of the mirror.

Systems And Methods For Launching A Plurality Of Spacecraft

View page
US Patent:
20200270001, Aug 27, 2020
Filed:
Feb 22, 2019
Appl. No.:
16/283396
Inventors:
- Chicago IL, US
Gary E. Lemke - Torrance CA, US
Jason D. Flathom - Irvine CA, US
Jeffrey S. Noel - Torrance CA, US
Assignee:
The Boeing Company - Chicago IL
International Classification:
B64G 1/64
B64G 1/00
Abstract:
Systems and methods for launching a plurality of spacecraft, provided in a stack of spacecraft, from a launch vehicle traveling along an in-track path include releasing, in a first separation event occurring at a first time, a first spacecraft from the stack of spacecraft using a first separation force having a first separation force in-track component along the in-track path. Subsequently, in a second separation event occurring at a second time, a second spacecraft is released from the stack of spacecraft using a second separation force having a second separation force in-track component along the in-track path, wherein the second time occurs a first time delay after the first time. The first and second separation in-track components may be different, such as by varying a magnitude of the separation force or an angle at which the spacecraft is launched.

Systems And Methods For Deploying Spacecraft

View page
US Patent:
20200024010, Jan 23, 2020
Filed:
Jun 3, 2019
Appl. No.:
16/430058
Inventors:
- Chicago IL, US
Jason D. Flathom - Irvine CA, US
Gary E. Lemke - Torrance CA, US
Dennis Yoichi Nakasone - Redondo Beach CA, US
Christopher P. Volk - Manhattan Beach CA, US
Elvis D. Silva - Denver CO, US
International Classification:
B64G 1/64
B64G 1/00
B64G 1/10
Abstract:
In an example, a spacecraft system includes a plurality of spacecraft in a stack. The stack has one or more layers, each layer includes at least two spacecraft, and each spacecraft is releasably coupled to one or more adjacent spacecraft in the stack. The spacecraft system also includes a controller configured to, for each layer, (i) cause the layer to release from the stack, and (ii) after the layer releases from the stack, cause the at least two spacecraft in the layer to release from each other.

Dual Condenser Loop Heat Pipe For Satellites With Sun-Normal Radiators

View page
US Patent:
20180222605, Aug 9, 2018
Filed:
Feb 3, 2017
Appl. No.:
15/424599
Inventors:
- Chicago IL, US
Jason D. Flathom - Chicago IL, US
Jonathan M. Allison - Chicago IL, US
Aimen E. Shawki - Chicago IL, US
Assignee:
THE BOEING COMPANY - Chicago IL
International Classification:
B64G 1/50
F28D 15/02
Abstract:
Systems, methods, and apparatus for dual condenser loop heat pipes for satellites with sun-normal radiators are disclosed. In one or more embodiments, a disclosed method for a satellite thermal management system comprises heating, in an evaporator, a liquid to convert the liquid to a vapor. The method further comprises passively circulating within tubing, from the evaporator, the vapor to a first radiator not illuminated by a sun and to a second radiator illuminated by the sun. Also, the method comprises converting the vapor to the liquid when the vapor is within the first radiator not illuminated by the sun. Further, the method comprises passively circulating within the tubing, from the first radiator not illuminated by the sun, the liquid to the evaporator.

Systems And Methods For Deploying Spacecraft

View page
US Patent:
20180162561, Jun 14, 2018
Filed:
Dec 8, 2016
Appl. No.:
15/373166
Inventors:
- Chicago IL, US
Jason D. Flathom - Irvine CA, US
Gary E. Lemke - Torrance CA, US
Dennis Yoichi Nakasone - Redondo Beach CA, US
Christopher P. Volk - Manhattan Beach CA, US
Elvis D. Silva - Denver CO, US
International Classification:
B64G 1/64
B64G 1/00
B64G 1/10
Abstract:
In an example, a spacecraft system includes a plurality of spacecraft in a stack. The stack has one or more layers, each layer includes at least two spacecraft, and each spacecraft is releasably coupled to one or more adjacent spacecraft in the stack. The spacecraft system also includes a controller configured to, for each layer, (i) cause the layer to release from the stack, and (ii) after the layer releases from the stack, cause the at least two spacecraft in the layer to release from each other.
Control profile
Jason D Flathom from Irvine, CA, age ~50 Get Report