Loads & Dynamics Engineer – Lead
Posted on 2/23/2023
Boom Supersonic

51-200 employees

Commercial supersonic airplane manufacturer
Company Overview
Boom Supersonic’s mission is to make the world dramatically more accessible. The company is developing supersonic aircrafts to enable cities that are rarely visited to become major travel destinations, let people attend meetings in far-off places and return for evenings with their loved ones, have global leaders solve crises in person, and let children grow up in a world where nothing is foreign.
Centennial, CO, USA
Experience Level
Desired Skills
Software Engineering
  • Bachelor, Master or Doctorate of Science degree in engineering with 15 or more years of experience in aerospace or an equivalent combination of technical education and aerospace experience
  • 10+ years of experience in a relevant aircraft product development role
  • Experience with certifying a Part 23/25 commercial aircraft. Knowledge of Part 23/25 sections relevant to loads and flutter, including AC 25.629. Experience coordinating with the FAA
  • Knowledge in planning for multiple load cycle development
  • Experience leading an analysis team of loads, dynamics, and flutter engineers
  • Knowledge of industry standard procedures for static/ dynamic loads, and flutter
  • Experience with fly-by-wire aircraft and aeroservoelastic implications
  • Supersonic delta wing experience
  • Nastran/Zaero experience
  • Experience with Ground Vibration Testing (GVT)/ Structural Coupling Testing (SCT)
  • Develop certification plan, means of compliance, and interpret issue papers related to loads and flutter
  • Collaborate across key disciplines (mass properties, flight controls, propulsion, flight sciences, structures, etc) to develop data needed for the aircraft loads in support of multiple load cycles
  • Guide team efforts on the development and maturation of static loads, dynamic flight loads (gust), dynamic ground loads (landing), and flutter analysis procedures to support downstream design and certification efforts
  • Ability to apply knowledge of aeroelasticity principles to develop aircraft conceptual design guidance