John Furumo Email & Phone Number

Lanham, Maryland, United States

Developing flight dynamics ground systems for NASA Goddard's OSAM-1 mission.

Simi Valley, CA

-Managed documentation and build records for fabrication of composites flight unit hardware for Mars Helicopter as part of AV team subcontracted to JPL for Mars 2020 mission. -Also performed structural testing of composites flight model hardware for Mars Helicopter, including static load destructive tests and design validation modal testing. -Helped design.

Greater Los Angeles Area

Product/Project engineer responsible for RS-68 rocket engine systems hardware including valves,ducts, flex lines, and harnesses.-Led corrective action team to investigate and find solutions to recurring harness security issues.-Assisted investigation of faulty hydraulic servo valves with suppliers and helped work containmentactivities including creating.

Camarillo, CA

Mechanical design engineer developing a test stand for qualification of dual-release lanyard (DRL) style and low separation force quick-disconnect electrical connectors for NASA’s Orion spacecraft.- Designed and fabricated pneumatic driven linear deployment fixture for separation testing of DRL style connectors using off-the-shelf components to minimize.

Hawthorne, CA

Manufacturing engineer engaged in production of carbon fiber composites flight hardware from both a process and product-driven focus.- Facilitated development of Falcon 9 Stage 2 Common Dome Insulation from first article to production-ready assembly and doubled production rate from 1 to 2 cores per month by driving design modifications for.

Hawthorne, CA

Manufacturing engineer engaged in production of Dragon spacecraft GNC Bay deployable mechanism, including fabrication, integration, and qualification and acceptance testing at the component, subassembly, and system level.- Worked with designers and suppliers to improve preexisting component design for manufacturability and integrability, finding solutions.

Hawthorne, CA

Thermal engineer engaged in improved component design for Dragon spacecraft thermal control system as well as creating fixtures and setups for various component qualification and acceptance tests as required for development and production application.- Designed a prototype valve body that combined four preexisting 3-way mixing and diverting valves in the.

Huntsville, AL

Engineering analyst assigned to ES22 Thermal and Mechanical Analysis Group for development of various launch vehicles and satellites in work at MSFC.- Utilized Altair HyperWorks CAE software package, along with X-TOOLSS genetic algorithm software to perform structural and thermal analysis and optimization on the next iteration of the FASTSAT project in.

Master Of Engineering - Meng, Aerospace, Aeronautical And Astronautical Engineering, Gpa 3.68

B.S., Mechanical Engineering, Gpa 3.45

Education record