Heather Kline, PhD

Technical Lead, advanced systems engineer/aerothermodynamicist, and mission control operator at Virgin Galactic
  • Claim this Profile
Contact Information
us****@****om
(386) 825-5501
Location
Tustin, California, United States, US

Topline Score

Topline score feature will be out soon.

Bio

Generated by
Topline AI

You need to have a working account to view this content.
You need to have a working account to view this content.

Credentials

  • Private Pilot License
    Federal Aviation Administration
    Mar, 2019
    - Nov, 2024

Experience

    • United States
    • Aviation and Aerospace Component Manufacturing
    • 700 & Above Employee
    • Technical Lead, advanced systems engineer/aerothermodynamicist, and mission control operator
      • Apr 2020 - Present

      • Led implementation of Multi-Disciplinary Analysis and Optimization, demonstrating its capabilities to chief engineers and applied to trade studies. • Gained leadership experience through acting as a liason between the flight sciences department and chief engineering for VSS Imagine, training of new console operators, and leadership of projects within the advanced systems department. • Evaluated transient aerothermodynamics analysis for SpaceShip TPS design. • Participated in… Show more • Led implementation of Multi-Disciplinary Analysis and Optimization, demonstrating its capabilities to chief engineers and applied to trade studies. • Gained leadership experience through acting as a liason between the flight sciences department and chief engineering for VSS Imagine, training of new console operators, and leadership of projects within the advanced systems department. • Evaluated transient aerothermodynamics analysis for SpaceShip TPS design. • Participated in requirements definitions and program planning efforts. • Gained high-pressure mission control experience as a console operator and trainer for flight test campaigns. • Mentored others in my organization both through training for specific technical tools and in broader professional skills. • Provided analysis and design for a commercial high-speed transport concept, evaluating supersonic inlets, aerothermodynamics, and sonic booms. Show less • Led implementation of Multi-Disciplinary Analysis and Optimization, demonstrating its capabilities to chief engineers and applied to trade studies. • Gained leadership experience through acting as a liason between the flight sciences department and chief engineering for VSS Imagine, training of new console operators, and leadership of projects within the advanced systems department. • Evaluated transient aerothermodynamics analysis for SpaceShip TPS design. • Participated in… Show more • Led implementation of Multi-Disciplinary Analysis and Optimization, demonstrating its capabilities to chief engineers and applied to trade studies. • Gained leadership experience through acting as a liason between the flight sciences department and chief engineering for VSS Imagine, training of new console operators, and leadership of projects within the advanced systems department. • Evaluated transient aerothermodynamics analysis for SpaceShip TPS design. • Participated in requirements definitions and program planning efforts. • Gained high-pressure mission control experience as a console operator and trainer for flight test campaigns. • Mentored others in my organization both through training for specific technical tools and in broader professional skills. • Provided analysis and design for a commercial high-speed transport concept, evaluating supersonic inlets, aerothermodynamics, and sonic booms. Show less

    • Research And Development Engineer
      • May 2017 - Mar 2020

      • Derived and implemented boundary layer stability for thermochemical nonequilibrium for LST, PSE, and NLPSE in 2 and 3 dimensions in the Langley Stability and Transition Analysis Code (LASTRAC). • Expanded project requirements to add a flexible interface for arbitrary chemistry models. • Derived and implemented boundary layer stability for thermochemical nonequilibrium for LST, PSE, and NLPSE in 2 and 3 dimensions in the Langley Stability and Transition Analysis Code (LASTRAC). • Expanded project requirements to add a flexible interface for arbitrary chemistry models.

    • United States
    • Higher Education
    • 700 & Above Employee
    • NASA Space Technology Research Fellow / Graduate Student
      • Mar 2012 - May 2017

      I was a recipient of the NASA Space Technology Research Fellowship for the maximum of 4 years, and through this fellowship I worked at multiple NASA sites as a 'Visiting Technologist'. Further detail is listed in separate experience entries. This fellowship allowed me to complete a PhD in the Aerospace Design Laboratory at Stanford University, working with Professor Juan Alonso. As a PhD candidate in the Aerospace Design Laboratory, I worked to develop methods related to the continuous… Show more I was a recipient of the NASA Space Technology Research Fellowship for the maximum of 4 years, and through this fellowship I worked at multiple NASA sites as a 'Visiting Technologist'. Further detail is listed in separate experience entries. This fellowship allowed me to complete a PhD in the Aerospace Design Laboratory at Stanford University, working with Professor Juan Alonso. As a PhD candidate in the Aerospace Design Laboratory, I worked to develop methods related to the continuous adjoint method aimed at optimizing hypersonic inlets. I am a developer on SU2, an open source Computational Fluid Dynamics and Multi-Physics Simulation tool developed in this lab. Show less I was a recipient of the NASA Space Technology Research Fellowship for the maximum of 4 years, and through this fellowship I worked at multiple NASA sites as a 'Visiting Technologist'. Further detail is listed in separate experience entries. This fellowship allowed me to complete a PhD in the Aerospace Design Laboratory at Stanford University, working with Professor Juan Alonso. As a PhD candidate in the Aerospace Design Laboratory, I worked to develop methods related to the continuous… Show more I was a recipient of the NASA Space Technology Research Fellowship for the maximum of 4 years, and through this fellowship I worked at multiple NASA sites as a 'Visiting Technologist'. Further detail is listed in separate experience entries. This fellowship allowed me to complete a PhD in the Aerospace Design Laboratory at Stanford University, working with Professor Juan Alonso. As a PhD candidate in the Aerospace Design Laboratory, I worked to develop methods related to the continuous adjoint method aimed at optimizing hypersonic inlets. I am a developer on SU2, an open source Computational Fluid Dynamics and Multi-Physics Simulation tool developed in this lab. Show less

    • United States
    • Aviation and Aerospace Component Manufacturing
    • 700 & Above Employee
    • Visiting Technologist
      • Jun 2015 - Sep 2015

      As a portion of the NASA Space Technology Research Fellowship, I ran unsteady CFD simulations using SU2, and modified MATLAB scripts, both in support of wind tunnel tests. As a portion of the NASA Space Technology Research Fellowship, I ran unsteady CFD simulations using SU2, and modified MATLAB scripts, both in support of wind tunnel tests.

    • Visiting Technologist
      • Jun 2014 - Aug 2014

      As a portion of a NASA Space Technology Research Fellowship I implemented interpolation routines for fluid-structure interactions using Fortran90. As a portion of a NASA Space Technology Research Fellowship I implemented interpolation routines for fluid-structure interactions using Fortran90.

    • United States
    • Aviation and Aerospace Component Manufacturing
    • 700 & Above Employee
    • Visiting Technologist
      • Jun 2013 - Aug 2013

      As a portion of the NASA Space Technology Research Fellowship, I conducted CFD simulations and mesh deformation to produce a response surface of various quantities of interest on a hypersonic inlet. As a portion of the NASA Space Technology Research Fellowship, I conducted CFD simulations and mesh deformation to produce a response surface of various quantities of interest on a hypersonic inlet.

    • United States
    • Defense and Space Manufacturing
    • 700 & Above Employee
    • Intern
      • Jun 2011 - Aug 2011

      My responsibilities included python code development and spacecraft dynamics simulation with DSENDS. My responsibilities included python code development and spacecraft dynamics simulation with DSENDS.

    • United States
    • Aviation and Aerospace Component Manufacturing
    • 700 & Above Employee
    • Intern
      • Jun 2010 - Aug 2010

      During this internship as part of the Aeronautics Scholarship Program, I conducted CFD simulations for a transonic airfoil with active flow control. During this internship as part of the Aeronautics Scholarship Program, I conducted CFD simulations for a transonic airfoil with active flow control.

Education

  • Stanford University
    Doctor of Philosophy (PhD), Aerospace, Aeronautical and Astronautical Engineering
    2013 - 2017
  • Stanford University
    Master's degree, Aerospace, Aeronautical and Astronautical Engineering
    2011 - 2013
  • Rensselaer Polytechnic Institute
    Bachelor of Science (BS), Dual Aerospace & Mechanical Engineering
    2007 - 2011

Community

You need to have a working account to view this content. Click here to join now