2021–Present Zipline, Staff Engineer - Aerodynamics, Aircraft Design and Multidisciplinary Optimization
2019–2021 Amazon Prime Air, Applied Scientist II - Aircraft Design and Multidisciplinary Optimization
2014–2019 University of Washington, Aeronautics & Astronautics, PhD Research Assistant
2014–2017 NASA, Ames Research Center, Research Engineer
2012–2014 University of Illinois at Urbana-Champaign, Aerospace Engineering, Graduate Research Assistant
2011–2012 Embraer, Product Development Engineer - Applied Aerodynamics and Flight Mechanics
2008 (summer) Massachusetts Institute of Technology, Mechanical Engineering, Summer Undergraduate Research Assistant
2006–10 University of Sao Paulo, SAE Aero Design Competition, Undergraduate Student Competitor
2021-Present Zipline
Zipline International
Mission: create the first logistics system that serves all humans equally.- Configuration: electric aircraft- Fixed-Wing and - Vertical Takeoff and Landing (eVTOL)- More information: Zipline International2019-2021 Amazon Prime Air
Amazon Prime Air
- Configuration: electric Vertical Takeoff and Landing (eVTOL) aircraft- Mission: drone for 30-min package delivery- More information: Amazon Prime Air2014-2017 NASA - Ames Research Center
Subsonic Ultra-Green Aircraft Research (SUGAR)
- Configurations:2011-2012 Embraer KC-390
EMBRAER's largest airplane ever designed and built
- Configuration: high-swept-wing / T-tail- Mission: multi-mission tactical transport aircraft Troop and cargo transport / Air delivery / Aerial refueling / Search and rescue / Forest fire fighting / Disaster relief / Humanitarian aid operations)- Crew: 2- Capacity: 80 passengers or 64 airborne troops or 6 pallets (68"x108") or 74 litter patients- Payload: 26 tonnes (59,500 lb)- Length: 33.43 m (109 ft 8 in)- Wingspan: 33.94 m (111 ft 4 in)- Height: 11.43 m (37 ft 6 in)- Max. takeoff weight: 81.0 tonnes (178,574 lb)- Powerplant: 2 × IAE V2500-E5 turbofan, 139.4 kN (31,330 lbf) each- Maximum speed: Mach 0.8 (470 knots, 850 km/h, 541 mph)- Range: 2,730 nmi (5,055 km) (with 14 ton payload) - Service ceiling: 36,000 ft (10,973 m)2011 "Penguin"
8th place overall (90+ teams)
- Configuration: flying wing- Payload: 11.865 kg- Empty Weight: 3.9 kg- Structural efficiency ratio: 3.04- Engine: OS .612010 "Tuiuiu"
4th place overall / Highest Payload World Record / Best Payload Unloading Time / Best Accuracy / First Competitive Flying Wing (90+ teams)
- Configuration: flying wing- Payload: 16.215 kg- Empty Weight: 3.745 kg- Structural efficiency ratio: 4.33- Span: 3.80 m- Engine: OS .612009 "BR 2009"
6th place overall (90+ teams)
- Configuration: monoplane- Payload: 10.3 kg- Empty Weight: 2.3 kg- Structural efficiency ratio: 4.48- Span: 2.30 m- Engine: OS .612009 "Pelican"
1st place overall / Highest Payload Honor / NASA Systems Engineering Award for Best Project (60+ international teams)
- Configuration: blended-wing body /monoplane, twin tailboom- Payload: 12.841 kg- Empty Weight: 2.7 kg- Structural efficiency ratio: 4.76- Span: 2.30 m- Engine: OS .612008 "Frango"
2nd place overall / Best Payload Unloading Time (90+ teams)
- Configuration: low-wing monoplane, twin tailboom, H-Tail- Payload: 11.365 kg- Empty Weight: 3.3 kg- Structural efficiency ratio: 3.44- Span: 3.20 m- Engine: OS .612007 "Caçador"
9th place overall (90+ teams)
- Configuration: swept-wing monoplane w/ winglets, Fowler flaps, U-Tail- Payload: 9.950 kg- Empty Weight: 2.7 kg- Structural efficiency ratio: 3.69- Span: 2.40 m- Engine: OS .612007 "Drosophila"
8th place overall (60+ international teams)
- Configuration: conventional monoplane- Payload: 10.6 kg- Empty Weight: 2.2 kg- Structural efficiency ratio: 4.82- Span: 2.20 m- Engine: OS .612006 "Galinha"
1st place overall / Highest Payload Honor (90+ teams)
- Configuration: box-wing biplane- Payload: 12.135 kg- Empty Weight: 3.6 kg- Structural efficiency ratio: 3.37- Span: 2.40 m- Engine: OS .61Aircraft Design: Awards / Records / Trophies
A2 - Wind Tunnel, Mooresville, NC - USA
University of Washington - Wind Tunnel, Seattle, WA - USA
Wichita State University - Wind Tunnel, Wichita, KS - USA
NASA - Icing Research Tunnel (IRT), Cleveland, OH - USA
German-Dutch Wind Tunnels (DNW) Large Low-Speed Facility (LLF), Marknesse, Netherlands
Instituto de Pesquisas Tecnológicas (IPT), Sao Paulo, Brazil
Private Pilot
Piper Archer III
Cessna 172
Hang Gliding Pilot