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Mr. William W. WangHome Phone No. 805-492-2841Personal Email Address: [email protected] Engineering Specialist
Years of Experience: 40
Years at Analex: 2
Years at Aerospace: 26
Experience Summary Propulsion Panel Lead for National Reconnaissance Office Mission Assurance Team
for all NRO Missions 2000 – now Member of MDA EKV Failure Review Board 2011-2012 Served on National Research Council independent assessment of NASA’s
Exploration Technology Development Program (ETDP), 2007-2008 Team member on NESC Independent Review the Space Shuttle and International
Space Station Programs’ Recurring Anomalies, 2005 Led Aerospace Team Review of Air Force Rocket Laboratory A-1 Test Stand for RS-
68 Testing, 1997 Led the Titan IV Stage II Ablative Nozzle Failure Recovery Testing at Arnold
Engineering & Development Center in 1996. Led AC-70 & AC-71 Flight Failures RL-10 Return-to-Flight Testing at Pratt &
Whitney, West Palm Beach in1993.
Work Experience Analex/Vencore (2013 to now)
Continue mission assurance role for NRO missions on Delta IV and Atlas V. Follow SpaceX propulsion development.
The Aerospace Corporation (1987 to 2013)
Perform Propulsion Support and Analysis for Titan, Atlas, Delta, EELV Liquid Propulsion Systems. Perform Planning, Testing, and Data Analysis for RL-10 Engines, Titan II & IV Engines, Atlas II & V Engines, and Delta II Engines. As Mission Assurance Team Panel Lead, added responsibility to support Real Time Risk Assessment on all Propulsion Issues during Launch Processing
Rocketdyne, Canoga Park, CA. (1975-1987)
Mr. William W. WangPage 1
Development Engineer. Designed and Tested a Pressurized Pulverized Coal Combustor using Rocket Injector
TechnologyDesigned a Fluidized Bed Coal Combustion/Heater Designed and Tested a LOX/CH4 Preburner Designed Acoustic Cavities for Gas Dynamic Laser Gas Generator, Peace Keeper
Axial Engine and Attitude Control Engines for Combustion Stability
System Project Engineer LS-14
System Analyst for the following projects: Solar-1 Project, Mini Kill Vehicle Propulsion System, Torpedo Ejector System, Engine Start Transients Simulation for XLR-132, SSME, LOX/Hydrocarbon Engines, Sonar Pulse Engine
Education M.E.E. Engineering Executive Program, University of California Los Angeles, Los
Angeles, CA M.A.A Aeronautics and Astronautics, University of Washington, Seattle, WA M.S. Aeronautics and Astronautics, University of Washington, Seattle, WA B.S. Aeronautics and Astronautics, University of Washington, Seattle, WA
Relevant Coursework Thermodynamics Gas Dynamics Fluid Mechanics Boundary Layer Theory Aerodynamics Structures Laser Physics Design and Testing of Gas Turbines and Airplanes
Technical Skills Digital and Analog Computer Programming Non-Destructive Testing
Mr. William W. WangPage 2
Professional Societies, Honors, Awards Associate Fellow, AIAA Industrial Partner Awards NRO/OSL Group Achievement Award, NASA Engineering and Safety Center Going The Distance Award for Outstanding Contribution to the RL-10 Engine Test
Program, USAF Group Achievement Award for Outstanding Development of a Uniquely
Comprehensive Centaur Rocket Engine Transient Model
Publications Year in Review, Liquid Propulsion, Aerospace America, December 2005, 2006, 2007 Co-authors “Space System Modeling and Simulation: Roles and Applications
Throughout the System Life Cycle”. Aerospace Press, 2002
Mr. William W. WangPage 3
