Terrill L. Burlison

PO Box 5246
Kent WA 98064
(425) 413-1371 (home)
tburlison @this domain

(Click here for a shorter, printer-friendly version of this resume)

"Reality must take precedence over public relations, for Nature cannot be fooled."
--Richard Feynman

I Am Seeking:

A position as a lead trajectory/performance analyst or software/simulation developer at a firm involved in the design, development, or operation of aerospace systems. I have a particular interest in manned spaceflight systems or rendezvous and proximity operations.

What I Offer:

I have consistently provided guidance and leadership in identifying needs (and solutions) in areas within and beyond my specified work area. My work is original, creative, and thorough, and I am not afraid to challenge established preconceptions. Not only do I accept responsibilities assigned to me, but I undertake new responsibilities on my own initiative.

My former lead at Kistler recently told me, "If everyone had shown the creativity and quality in their work as you, we might have succeeded."


My Skills

Aerospace: Computers: Business:

I am also a published writer of fiction, non-fiction, and technical subjects. I work well on my own or with others. I am dependable, hard working, and a quick study. I am a long-time member of: Air & Space Smithsonian, The Planetary Society, and the National Space Society (from whom I received a Top Recruiter award for 1997). I am married to Linda Burlison (also an aerospace/software engineer), and we have two children.


My References (contact info available upon request)

Kistler:

Boeing/NASA:


My Background

Purdue University
1974-1979
I graduated with a degree in Aeronautical and Astronautical Engineering from Purdue University in 1979. I was elected to the Tau Beta Pi engineering honor society and the Sigma Gamma Tau aerospace engineering honor society. I majored in Astronautics with a minor in Propulsion. I also had a minor in Mathematics.
NASA JSC
1979-1982
I joined the National Aeronautics and Space Administration in 1979. I worked at the Johnson Space Center (JSC) in Houston, Texas, as a Flight Dynamics Officer (FIDO) in the Mission Control Center (MCC). As a flight controller, my duties included:
  • Real-time flight operations:
    • Monitoring shuttle trajectory
    • Planning and uplinking deorbit maneuvers
    • Maintaining shuttle ground ephemeris
  • Simulation development:
    • On-orbit maneuver simulations
    • Rendezvous planning and analysis
  • Developing mission operations code for the Emergency Mission Control Center
  • Developing Mission Operations guidelines
  • Determining MCC rendezvous processor requirements and designing the displays (still in use today)
  • Developing on-orbit emergency procedures
Boeing
1982-1992
In 1982, I went to work for Boeing Aerospace in Kent, Washington, where I worked on projects such as Orbital Maneuvering Vehicle (OMV), Inertial Upper Stage (IUS), Lunar Scout, Expendable Launch Vehicle (ELV), and Silencer. My responsibilities included:
  • Rendezvous mission analysis and planning
  • Simulation development
  • Satellite constellation design and analysis
  • Lunar mission trade studies
  • Guidance system mission design
  • Real-time flight operations at the Satellite Control Facility (now Onizuka AFS) in Sunnyvale, CA
  • Presenting my work to the Pentagon, Army Intelligence Command, NASA-Huntsville, Kirtland Air Force Base, and other customers.
Six String Software
1992-1998
In 1992, I started my own company for developing and publishing software for home PCs. Six String Software has produced over a dozen music and game products, receiving very favorable reviews from national publications. As president/owner, I am responsible for all aspects of product development and business operations, including:
  • Product design
  • User interface design
  • Programming and testing
  • Hiring and overseeing contract employees
  • Budgeting
  • Scheduling 
  • Marketing and promotion (writing press releases, giving demos, etc.)
  • Sales 
Andrews Space & Technology
2002-2003
Contracted with Andrews Space & Technology. My responsibilities included:
  • Launch window analysis
  • Rendezvous design
  • Interfacing with Draper Labs to assure compliance with NASA requirements
  • Presenting results to Marshall Space Flight Center
Kistler Aerospace
1999-2005
In March 1999, I joined Kistler Aerospace as a contract engineer. In September 2004, I joind the full-time staff as Flight Dynamics lead. My responsibilities included:
  • Trajectory and performance analysis
  • Developing rendezvous procedures and requirements for ISS resupply and other potential missions
  • Launch window analysis and rendezvous design
  • Developing trajectory tools using Fortran, C++, and Microsoft Foundation Classes (MFC)
  • Interfacing with subcontractors
LTS
2005
Upon Kistler's shutdown, I contracted with Bob Citron and Walter Kistler at Lunar Transportation Systems to provide analyses to support their lunar mission architecture. My responsibilities included:
  • Lunar trajectory and performance analysis
  • Developing rendezvous procedures and requirements to support the LTS architecture
  • Adapting the vehicle design to fit the dynamic envelope of the Delta II launch vehicle
  • Overseeing and managing the subcontractor (IN Space, LLC) who provided the attitude jet design
RpK
2006
In January 2006, Rocketplane, Ltd. and Kistler Aerospace merged. I contracted with the new company, Rocketplane-Kistler, as acting Deputy Program Manager for Mission Operations. I was the primary technical writer for NASA's Commercial Orbital Transportation Services (COTS) Demonstration proposal, and provided virtually all technical analysis and deliveries during the eight month proposal effort. My work was deemed critical by NASA's technical review committee, culminating in RpK's $207 million award. My responsibilities included:
  • Delivering numerous briefings, documents, and analyses to NASA
  • Performing trajectory, loads, and thermal analyses for ascent/rendezvous/entry and aborts
  • Defining manned and unmanned vehicle specifications and operational procedures
  • Developing training and mission operations requirements
  • Defining evolved vehicle concepts to meet future heavy-lift and Exploration needs (LEO, lunar, Mars)
  • Verifying the RpK COTS vehicle would meet NASA ISS interface and systems requirements