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Propulsion Engineer -Aerospace Engineering (NASA Sounding Rocket Program)

2024-150885
Engineering
No Clearance

Location:

Wallops Island
,
VA

Secondary Location:

,
,

Telecommute Options:

Flexible for occasional telework – must be local to work location
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About Peraton

Peraton is a next-generation national security company that drives missions of consequence spanning the globe and extending to the farthest reaches of the galaxy. As the world’s leading mission capability integrator and transformative enterprise IT provider, we deliver trusted, highly differentiated solutions and technologies to protect our nation and allies. Peraton operates at the critical nexus between traditional and nontraditional threats across all domains: land, sea, space, air, and cyberspace. The company serves as a valued partner to essential government agencies and supports every branch of the U.S. armed forces. Each day, our employees do the can’t be done by solving the most daunting challenges facing our customers. Visit peraton.com to learn how we’re keeping people around the world safe and secure.

Responsibilities

NASA’s Sounding Rocket Operations Contract (NSROC) is a sub-orbital space flight program located at NASA’s Wallops Flight Facility (WFF), a part of NASA’s Goddard Space Flight Center (GSFC). NSROC provides suborbital launch vehicles, payload development and field operations support to NASA’s Science Mission Directorate. The program enables the collection of Earth, Heliophysics and Astrophysics science.

 

This position will require an individual to be able to work individually and work in a team environment. Applicant will be in the Launch Vehicle Engineering group for sounding rocket missions. The application will support mechanical design and testing of standard launch vehicle systems components. This position will require an individual to be locally located to support efforts on base as well as be able to support required telework. Applicant will work on a variety of projects, typically multiple at any one time.

 

The Launch Vehicle Engineer (Propulsion) applies mechanical, thermal dynamics, and fluid dynamics principles to components and systems, including assembly, analysis, and documentation of results; construction of developmental assemblies, sub-assemblies and components; and quality testing. Supports and participates in the design, test, modification, fabrication and assembly of launch vehicle systems. is responsible for the design, testing and field operations support related to sounding rocket vehicle systems including flight termination, recovery, and stage ignition/separation. They research, develop, design, and test vehicle related components, equipment, and systems; applying principles and techniques of aerospace engineering. They are responsible for the production and presentation of technical material in support of internal and external customer meetings.

 

Responsibilities may include:

  • Supporting sub-orbital rocket launches by engineering vehicle systems and flight termination systems.
  • Analysis of solid rocket motor dynamics.
  • Developing and revising procedures and processes related to hazardous operations involving pyrotechnic devices, ordnance, and solid rocket motors.
  • Operate sounding rocket vehicle systems ground support equipment (GSE) during payload integration and testing, launch operations, and throughout suborbital flight.
  • Working in a fast-paced team environment performing launch vehicle hardware & software system and subsystem level integration, test and launch operation;
  • Troubleshooting, documenting and dispositioning flight and test equipment hardware and software discrepancies and pursuing root cause and corrective actions;
  • Executing and reviewing integration and test work packages;                                        
  • Conduct hazardous testing involving pyrotechnics.
  • Production and presentation of technical material in support of internal and external customer meetings.
  • Contribute to the development of new engineering products or specialty products, and specifications.
  • Participate in technical interchange discussions with customers and experimenters.
  • Manage the activities required to meet the objectives of assigned design and development projects.
  • Supporting the integration of, and transition to new hardware and software systems, and generating related documentation.
  • Serve as cognizant engineer for launch vehicles on NASA sounding rocket missions

 

 

 

Qualifications

Required Qualifications:

  • Bachelor's Degree or higher in a STEM discipline (Science, Technology, Engineering, Math) Aerospace Engineering, Mechanical Engineering, Chemistry, Chemical Engineering, Materials Science Engineering 
  • High mechanical and electrical aptitude
  • Ability to read, interpret, and implement technical drawings (electrical/mechanical), specifications, and procedures
  • Five years of engineering experience.
  • Knowledge of test instrumentation including, but not limited to, Power Supplies, DMMs, oscilloscopes, spectrum analyzers, and network analyzers, vibration tables, strength and bend testing,  etc.
  • An understanding of basic static and dynamic analysis related to flight structures.
  • Understanding of rocket motor dynamics

 

Ability to obtain a public trust

 

 

Desired Qualifications:

  • BS/MS Fluid Mechanics, Chemical Engineering, Chemistry
  • Experience in any of all of the following areas
    • Solid Rocket Motor Design and Analysis
    • SPP (Solid Performance Prediction) dynamic motor analysis
    • Solid Rocket propellant formulation
    • Solid rocket propellant grain manufacturing/ design
    • Solid rocket propellant grain inspection
    • Solid Rocket Motor testing /instrumentation / static fire
    • Hazardous Operation Procedure Creation
    • Rocket Motor Hazard Classification
    • MATLAB data analysis
  • Knowledge and familiarity of electronic and mechanical test equipment
  • Experience with ordnance systems involving solid rocket motors, initiators/igniters
  • Environmental test requirements and interpretation of test results for environments such as mechanical shock, random vibration, sine vibration, and acceleration.
  • Familiarity with hazardous operations and procedures.

 

#CivilSpace24

Target Salary Range

$104,000 - $166,000. This represents the typical salary range for this position based on experience and other factors.
SCA / Union / Intern Rate or Range

EEO

An Equal Opportunity Employer including Disability/Veteran.

Our Values

Benefits

At Peraton, our benefits are designed to help keep you at your best beyond the work you do with us daily. We’re fully committed to the growth of our employees. From fully comprehensive medical plans to tuition reimbursement, tuition assistance, and fertility treatment, we are there to support you all the way.

  • Paid Time-Off and Holidays
  • Retirement
  • Life & Disability Insurance
  • Career Development
  • Tuition Assistance and Student Loan Financing
  • Paid Parental Leave
  • Additional Benefits
  • Medical, Dental, & Vision Care
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