Posted 2w ago

Space Vehicle Attitude Control Systems Engineer

@ VTG
Chantilly, Virginia, United States
OnsiteFull Time
Responsibilities:monitoring progress, coordinating requirements, supporting testing
Requirements Summary:Active TS/SCI with polygraph; Bachelors (9+ yrs), Masters (7+ yrs), or PhD/JD (4+ yrs) in aerospace/astronautical/mechanical engineering; experience with spacecraft ACS hardware/software, DoD/IC acquisition, control theory, sensors/actuators, satellite bus design and launch/flight ops.
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Job Description
Overview

VTG is seeking a Space Vehicle Attitude Control Systems Engineer, in Chantilly, Va.


What will you do?

In this role, you will be responsible for monitoring, tracking, and reporting on progress & issues associated with spaceflight hardware currently in production and test for a classified space program.  You will be an integral participant in ACS and mechanical actuator design, requirements development & verification, and unit integration & test for a next generation spacecraft architecture.  

 

Job Duties include, but are not limited to: 

  • Review and coordinate changes to specifications, ICDs, and system level requirements documentation for ACS and propulsion subsystems.
  • Track development issues and attend unit, subsystem, system level design reviews.
  • Support launch and spacecraft on-orbit test, as required.
  • Identify and assess emerging risks and develops & evaluates proposed burn-down plans.
  • Review developer’s readiness to proceed into spacecraft test at various levels of assembly.

Do you have what it takes?

  • Active TS/SCI clearance with Polygraph
  • Bachelors Degree in Aerospace, Astronautical, or Mechanical Engineering and 9 years or more experience; Masters and 7 years or more experience; PhD or JD and 4 years or more experience. 
    • Desired education and experience with spacecraft ACS hardware and software design, manufacture, simulation, and test
  • Experience in DoD IC acquisition and program management processes.
  • Working knowledge of control theory, reaction wheel/control moment gyro, star sensor/tracker, inertial reference units/sensors, sun sensor, magnetic torque rod, GPS receiver, and control algorithm development. 
  • Experience in the design & integration of satellite buses and knowledgeable of launch & flight operations of space vehicles.
  • Ability to work collaboratively with personnel from multiple functions and at all levels of the customer organization to deliver results.