Propulsion Integration and Test RE II/III (Miranda Engine)

Posted 24 Days Ago
Be an Early Applicant
Briggs, TX, USA
In-Office
Mid level
Aerospace
The Role
Lead propulsion integration and test activities for liquid rocket engines: define configurations, design and execute test plans, analyze test data, mentor propulsion engineers, support manufacturability and production integration, and develop propulsion component concepts and test processes.
Summary Generated by Built In

ABOUT FIREFLY AEROSPACE

Firefly Aerospace is a space and defense technology company on a mission to reliably and repeatedly launch, land, and operate space systems from Earth to the Moon and beyond. As the partner of choice for critical space missions, Firefly is the first commercial company to launch a satellite to orbit with 24-hour notice and the first company to achieve a successful Moon landing. Headquartered in north Austin, Texas, Firefly is looking for passionate, hardworking innovators to join our team and help fuel our successful trajectory into space.

RESPONSIBILITIES

  • Collaborate with design, manufacturing, vehicle integration, production, and test operations teams to define engine configurations and support engine integration and test operations

  • Design and execute test plans supporting development, qualification, and flight engine test campaigns

  • Compile, interpret, and report on engine test data and evaluate performance relative to campaign and program objectives

  • Serve as a mentor for the existing propulsion engineers, providing technical guidance and leadership

  • Assist in developing new, innovative design concepts for propulsion components and experimental tooling, that reduce part count and complexity

  • Execute design for manufacturability changes to enhance production efficiency

  • Make development decisions based on technical merit, risk, cost, schedule, and/or quality assurance

  • Assist in the development of manufacturing, integration, and test processes, including work instructions, test procedures, and early build support

  • Partner with engineering and production teams to generate ideas, designs, and improvements for current and next-generation liquid rocket engines

QUALIFICATIONS

Required

  • Bachelor’s Degree in Mechanical Engineering, Aerospace Engineering, or equivalent

  • 3+ years of experience in a related aerospace or mechanical field, with a focus in propulsion or fluid systems

  • Experience leading technical reviews (design & analysis) or investigations (risk, anomaly, or trade studies)

  • Proven experience in data review, data analysis, and report generation

  • Experience in Siemens NX or equivalent CAD program

  • Understanding of bipropellant liquid rocket fundamentals and ability to collaborate with subject matter experts to maximize engine performance

  • Strong engineering fundamentals in compressible and incompressible flow, heat transfer, combustion devices, rocket engine cycles, and mechanics

  • Understanding of P&IDs, fluid system sizing, fluid component and instrumentation selection, fluid dynamics fundamentals, cryogenic systems and pressurized systems

  • Experience with maturing a conceptual design for use in a production environment

  • History of developing solutions with partially defined requirements and changing criteria.

Desired

  • MS or PhD in Mechanical or Aerospace Engineering

  • 5+ years of experience in a related aerospace or mechanical field, with a focus in propulsion or fluid systems

  • Strong interpersonal and organizational skills

  • Familiarity with presenting trade studies, risks, schedules, requirements, and budget to program management or leadership

  • Experience with liquid rocket engine development, design, test, or flight operations

  • Experience with liquid rocket engine subcomponent or pressurized component (valves, regulators, tubes, pipes, etc.) development, design, or test

  • A passion for product optimization design and rapid manufacturing

  • Hands-on experience with integrating test articles and sub-assemblies for test or production

  • Proven experience in working with data acquisition systems and test instrumentation including pressure transducers, thermocouples, resistance temperature detectors, flow meters, load cells, and accelerometers

  • Familiarity with some or all of the following software packages: Python, LabVIEW, GFSSP, Winplot, or other control, data acquisition, and reduction software

Firefly offers outstanding benefits for our employees, including generous health, dental and vision plans with low plan deductibles, parental leave, educational reimbursement, short term disability, and flexible PTO options.

To conform to U.S. Government space technology export regulations, including the International Traffic in Arms Regulations (ITAR) you must be a U.S. citizen, lawful permanent resident of the U.S., protected individual as defined by 8 U.S.C. 1324b(a)(3), or eligible to obtain the required authorizations from the U.S. Department of State.

Firefly Aerospace, Inc. is an Equal Opportunity Employer; employment with Firefly is governed based on merit, competence and qualifications and will not be influenced in any manner by race, color, religion, gender, national origin/ethnicity, veteran status, disability status, age, sexual orientation, gender identity, marital status, mental or physical disability or any other legally protected status

Skills Required

  • Bachelor's Degree in Mechanical Engineering, Aerospace Engineering, or equivalent
  • 3+ years of experience in a related aerospace or mechanical field, with a focus in propulsion or fluid systems
  • Experience leading technical reviews or investigations (design & analysis, risk, anomaly, or trade studies)
  • Proven experience in data review, data analysis, and report generation
  • Experience in Siemens NX or equivalent CAD program
  • Understanding of bipropellant liquid rocket fundamentals and ability to collaborate with subject matter experts
  • Strong fundamentals in compressible and incompressible flow, heat transfer, combustion devices, rocket engine cycles, and mechanics
  • Understanding of P&IDs, fluid system sizing, component and instrumentation selection, cryogenic and pressurized systems
  • Experience maturing a conceptual design for production use
  • History of developing solutions with partially defined requirements and changing criteria
  • MS or PhD in Mechanical or Aerospace Engineering
  • Strong interpersonal and organizational skills
  • Familiarity presenting trade studies, risks, schedules, requirements, and budget to leadership
  • Experience with liquid rocket engine development, design, test, or flight operations
  • Experience with liquid rocket engine subcomponent or pressurized component (valves, regulators, tubes, pipes) development, design, or test
  • Hands-on experience integrating test articles and sub-assemblies for test or production
  • Proven experience with data acquisition systems and test instrumentation (pressure transducers, thermocouples, RTDs, flow meters, load cells, accelerometers)
  • Familiarity with Python, LabVIEW, GFSSP, Winplot, or other control/data acquisition/reduction software
  • A passion for product optimization design and rapid manufacturing
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The Company
HQ: Cedar Park, TX
384 Employees
Year Founded: 2017

What We Do

Firefly Aerospace Inc. (”Firefly”) is developing a family of launch and in-space vehicles and services that provide industry-leading affordability, convenience, and reliability. Firefly’s launch vehicles utilize common technologies, manufacturing infrastructure, and launch capabilities, providing LEO launch solutions for up to ten metric tons of payload at the lowest cost per kg in the small-launch class. Combined with Firefly’s in-space vehicles, such as the Space Utility Vehicle and Blue Ghost lunar lander, Firefly will provide the space industry with a single source for missions from LEO to the surface of the Moon or beyond.

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