《飞行器系统工程》(英文版) Ron Suiter BSEE Lehigh

Ron Suiter. BSEE Lehigh. MBA USC Ron began his career as an aircraft system designer in Douglas Aircraft Companys Hydro-Mechanical system design group. He became Unit Chief of the braking system design group directly responsible for the design of the DC-9, DC-10, MD-80 anti-skid, auto-brake, brake temperature and tire pressure monitoring systems. He worked extensively with customers on design requirements, and with Flight Test and the FAA in design verification and certification. He was also the accident investigator for Douglas for all ground handling accidents Later on Presidents staff, Ron became the Senior Manager for Douglas's Company Operating Plans and later Strategic Plans. In that capacity he was given an assignment by the Cfo and VP Ops to understand the systemic causes of DAC's lack of profitability in the design and manufacture of commercial jets Returning to engineering, he assisted in the final certification of the MD-11 and as Director of Aircraft System design was responsible for Twin Jet and Trijet electrical, mechanical, hydraul fuel, and interior systems and headed up the Design Safety process team. Among many other initiatives Ron started a training program for aircraft system designers and the design for manufacturing(DFMA)initiative Ron completed his career at Boeing as the GM Product Definition for the C-17 Program in the Military Aircraft and Tankers Division. He was responsible for all Product Support and Engineering processes, Flight Test and Pilots groups Now as an independent consultant Ron has worked with the F-22 program, conducted studies of the systemic causes of expendable launch vehicle first launch failure, studied the causes of cost overruns in rlV programs, and is heading up the National Airspace System strategy simulator decision support project for the Federal Aviation Administration with Nextor Center of Excelle iversity participation including MIT
Ron Suiter, BSEE Lehigh, MBA USC Ron began his career as an aircraft system designer in Douglas Aircraft Company’s Hydro-Mechanical system design group. He became Unit Chief of the braking system design group directly responsible for the design of the DC-9, DC-10, MD-80 anti-skid, auto-brake, brake temperature and tire pressure monitoring systems. He worked extensively with customers on design requirements, and with Flight Test and the FAA in design verification and certification. He was also the accident investigator for Douglas for all ground handling accidents. Later on President’s staff, Ron became the Senior Manager for Douglas’s Company Operating Plans and later Strategic Plans. In that capacity he was given an assignment by the CFO and VP Ops to understand the systemic causes of DAC’s lack of profitability in the design and manufacture of commercial jets. Returning to engineering, he assisted in the final certification of the MD-11 and as Director of Aircraft System design was responsible for Twin Jet and Trijet electrical, mechanical, hydraulic, fuel, and interior systems and headed up the Design Safety process team. Among many other initiatives Ron started a training program for aircraft system designers and the design for manufacturing (DFMA) initiative. Ron completed his career at Boeing as the GM Product Definition for the C-17 Program in the Military Aircraft and Tankers Division. He was responsible for all Product Support and Engineering processes, Flight Test and Pilots groups. Now as an independent consultant Ron has worked with the F-22 program, conducted studies of the systemic causes of expendable launch vehicle first launch failure, studied the causes of cost overruns in RLV programs, and is heading up the National Airspace System strategy simulator decision support project for the Federal Aviation Administration with Nextor Center of Excellence university participation including MIT
按次数下载不扣除下载券;
注册用户24小时内重复下载只扣除一次;
顺序:VIP每日次数-->可用次数-->下载券;
- 《飞行器系统工程》(英文版) Propulsion Systems.pdf
- 《飞行器系统工程》(英文版)Aircraft Systems Engineering(Cost Analysis).pdf
- 《飞行器系统工程》(英文版) Commander Paul A. Sohl, USN.pdf
- 《飞行器系统工程》(英文版) PAUL ALFRED LAGACE.pdf
- 《飞行器系统工程》(英文版) Gordon mckinzie.pdf
- 《航空航天动力学》(英文版) Lecture 18 Aircraft Lateral dynamics.pdf
- 《航空航天动力学》(英文版) Lecture 17 Aircraft Longitudinal Dynamics.pdf
- 《航空航天动力学》(英文版) Lecture 16 Aircraft Dynamics.pdf
- 《航空航天动力学》(英文版) Lecture 15 SpaceCraf AHiud Dynamnics.pdf
- 《航空航天动力学》(英文版) LECTORE 14 GYRoScoPES.pdf
- 《航空航天动力学》(英文版) LECTORE 13 AXISYMMETRIC ROTATION S.pdf
- 《工程中的概率方法》Section5Article6.pdf
- 《工程中的概率方法》Section5Article9.pdf
- 《工程中的概率方法》compmethods.pdf
- 《工程中的概率方法》Section5Article8.pdf
- 《工程中的概率方法》Section5Article3.pdf
- 《工程中的概率方法》Section5Article4.pdf
- 《工程中的概率方法》Section5Article7.pdf
- 《工程中的概率方法》Section5Article5.pdf
- 《工程中的概率方法》Section3Article10.pdf
- 《飞行器系统工程》(英文版) SHUTTLE HISTORY.pdf
- 《飞行器系统工程》(英文版) Briefing Summary.pdf
- 《飞行器系统工程》(英文版) Lean Systems Engineering l l.pdf
- 《飞行器系统工程》(英文版) Aerodynamics Primer.pdf
- 《飞行器系统工程》(英文版) aircraft_murman.pdf
- 《飞行器系统工程》(英文版) Vice President/General Manager.pdf
- 《飞行器系统工程》(英文版) LECTURE OUTLINE.pdf
- 《飞行器系统工程》(英文版) Brian Kelly Bio.pdf
- 《飞行器系统工程》(英文版) AARON COHEN.pdf
- 《飞行器系统工程》(英文版) Today' s class.pdf
- 《飞行器系统工程》(英文版) Payload, Range and Speed.pdf
- 麻省理工学院:《Multidisciplinary System》Lecture 1 4 February 2004.pdf
- 麻省理工学院:《Multidisciplinary System》Lecture 3: Modeling and Simulation.pdf
- 麻省理工学院:《Multidisciplinary System》Lecture 4 17 February.pdf
- 麻省理工学院:《Multidisciplinary System》Lecture 2 9 February.pdf
- 麻省理工学院:《Multidisciplinary System》Lecture 5 18 February.pdf
- 麻省理工学院:《Multidisciplinary System》Lecture 6 23 February.pdf
- 麻省理工学院:《Multidisciplinary System》Issues in Optimization.pdf
- 麻省理工学院:《Multidisciplinary System》Lecture 7 25 February.pdf
- 麻省理工学院:《Multidisciplinary System》Lecture 8 1 March.pdf