Peraton Overview

Peraton drives missions of consequence spanning the globe and extending to the farthest reaches of the galaxy. As the worlds leading mission capability integrator and transformative enterprise IT provider, we deliver trusted and highly differentiated national security solutions and technologies that keep people safe and secure. Peraton serves as a valued partner to essential government agencies across the intelligence, space, cyber, defense, civilian, health, and state and local markets. Every day, our 22,000 employees do the cant be done, solving the most daunting challenges facing our customers.

Qualifications

Requires 2 to 5 years with BS/BA or 0 to 2 years with MS/MA/MBA or 8 to 10 years with no degree.

Active Secret Security Clearance or higher

Responsibilities

Responsible for conducting cost estimating, test planning and execution, data acquisition, data analysis and reporting on assigned flight-testing projects. Advise and guide other engineers and project officers in the testing of advanced rotary wing and fixed wing aircraft, to include the disciplines of aircraft performance, stability and control, propulsion, cockpit displays, and aircraft systems. Coordinate the application of scientific theory and engineering principles to the test and evaluation mission of the United States Army Aviation Technical Test Center. Apply standard technical skills to resolve problems that result from the test and evaluation of advanced rotary wing and fixed wing aircraft such as stability and control, propulsion, cockpit displays, and aircraft systems. Assist other engineers in the design and execution of tests, analysis of data, and reporting of results, including the interpretation of the significance of the findings. Must demonstrate the capability to publish reports and technical papers on the results of developmental and/or experimental flight testing of advanced rotary wing and fixed wing aircraft. Must have demonstrated the capability to compile, reduce, format, analyze and present test data. Must have demonstrated the ability to apply the practical knowledge of aerospace engineering to flight testing principles and concepts applicable to the developmental and system testing of rotary wing and fixed wing aircraft, performance, stability and control, vehicle dynamics and handling qualities. Must have demonstrated knowledge in the theory and applicability of aerodynamics and propulsion as they relate to the performance of rotary wing and fixed wing aircraft.