Design and development of space borne mechanisms and optical mounts for IR payloads.
Includes completing mechanical analysis, architecture definition design development with supporting trade studies.
Job will include being part of a team of engineers in accomplishing the above assignments.
Mechanical systems methods for IR payloads and subsystems from requirement allocations and flow downs to specification and interface definition and compliance verification.
Detailed mechanical design skills of mechanisms for payloads.
Collaborate with Manufacturing and Procurement during the build and test of mechanisms.
Author PDRs, CDRs, and other required design review documents.
Perform trade studies to determine optimal designs.
Complete mass, torque margin and tolerance budgets and current predictions.
Interface with team and other functions including Systems engineering, Operations and Quality.
Participate in risk assessment and develop mitigation strategies for complex projects.
Ability to obtain a U.S. Security Clearance.
Up to 10% travel may be required.
Requirements
Bachelor’s Degree and a minimum of 2 years of prior related experience.
Graduate Degree or equivalent with 0 to 2 years of prior related experience.
In lieu of a degree, minimum of 6 years of prior related experience.
Experience in design for testing in space environments (i.e., temperature, vacuum, radiation, etc.)
Professional experience in 3D CAD modeling
Strong hands-on capabilities, to include integration and diagnosis of mechanisms and products.
Active Security Clearance is preferred
PTC Creo or Solidworks strongly preferred
NASA 5017 and ABMA Standards knowledge
GD&T, tolerance stacks
Expertise in 3D CAD modeling
Excellent people skills, with collaborating in a multi-disciplinary, diverse, and dynamic team environment.
Prior mechanism design experience
Experience using Microsoft Office products.
Benefits
Relocation assistance is available to qualified applicants