David Ayala Email & Phone Number

El Segundo, CA, US

Hawthorne, California, United States

• Responsible for the CAD, drawings, manufacturing, inspection, assembly, and testing of the E2 injector components
• Documented and conducted assembly procedures of Lox pump and TCAs at NASA Stennis, reducing the assembly/disassembly of necessary plumbing, mounting, and electronics to 1 day
• Designed and manufactured tooling for engine repair, TCA assembly fixture, and E2 injector water flow test stand
• Redesigned injector component to introduce new manufacturing technique to reduce production time by 65%
• Introduced new quality assurance procedure to standardize verification & validation of component dimensions
• Conducted warpage study of 3D printed injector body through manufacturing process to reduce risk of part scrappage

Mojave, California, United States

• Developed drawings according to ASME Y14.5 for primary and secondary structures of the XL-1 Lunar Lander
• Designed in context secondary sheet metal mounting structures according to the Boeing Design Manual in Solidworks
• Conducted structural, frequency response, and topology studies to verify component performance and reduce mass
• Handled G-Ox/G-CH4 as ground crew for test campaign of 100 lbf engine, performing all necessary safety checks
• Part of disassembly/reassembly team for Xodiac’s 700 lbf engine, inspecting and cleaning components as needed

Austin, Texas Area

• Tasked with overseeing and maintaining the design and manufacturing of the recovery bay and the nosecone
• Ran 2D and 3D drag analyses with ANSYS Fluent on rocket to determine optimal fineness ratio of nosecone
• Designed, constructed, and successfully tested a pyrotechnic deployment system for a 6 ft drogue parachute
• Coupled 1 DOF re-entry model of rocket with parachute calculator in Python to create preliminary size of parachutes
• Developed a bolted joint calculator to determine margin of safety for each failure mode of a bolted joint design

My role at JPL entailed mechanical design and analysis for three key aspects of the test campaign of a new mechanism to be used on the Sample Return Lander in the Mars Sample Return Campaign. The first design test piece I developed was a mass model representing the Mars Ascent Vehicle (MAV). The mass model had to be modular in mass, moment of inertia, and.

New Haven, CT

Starting in January, my job was to develop an academic curriculum for students all over the US to better understand engineering and learn the basic skills that all engineers use. Additionally during the spring, I interviewed over 15 candidates and hired 8 candidates for the summer positions that I had to fill. These candidates were to be trained and.