Vetted SpecialistsExample profilePriya K.Senior Mechanical Design Engineer, Spacecraft StructuresOwned primary structure and deployable solar array mechanisms for a 400 kg ESPA-class bus from PDR through CDR; released 220+ drawings in NX and Teamcenter with two configuration-level changes after releaseCut structure mass 14% against allocation through machined-panel redesign and fastener consolidation while holding stiffness above the launch-vehicle first-mode requirementRan the tolerance stack and alignment budget for a star-tracker bracket that held 0.02 degrees of boresight knowledge through thermal-vacuum without post-test shimmingNX / TeamcenterGD&T Y14.5Deployables
Vetted SpecialistsExample profileKyle P.Mechanical Design Engineer, Launch Vehicle Fluids and StructuresDesigned the valve manifolds, feedline brackets and thrust-structure fittings for a small-lift vehicle stage in CATIA and 3DEXPERIENCE; first-article yield on his released parts above 90% across three vendorsConverted a 27-piece welded assembly to a single five-axis machined titanium part, removing 11 inspection points and four weeks from the build scheduleWrote the cryogenic fastener and coating standard now applied across the stage — A-286 and Inconel selection, dry-film lubricant callouts and passivation per AMS 2700CATIA / 3DXDFM / DFACryogenic materials
Vetted SpecialistsExample profileClarence T.Principal Mechanical Design Engineer, Defense SystemsLed mechanical design for a Group 3 UAS airframe and a seeker gimbal housing from concept to rate production in SolidWorks and Windchill, under DCMA oversight and ITAR controlOwned the transition to production for 600+ part numbers: DFM reviews with three machine shops, PPAP-style first articles, and a change process that stabilized the configuration inside two revisionsChaired 20+ design reviews across two programs; mentored a team of six design engineers and set the drawing and GD&T checking standard for the siteSolidWorks / WindchillTransition to productionDesign reviews