E-Space
Senior Electromechanical Engineer — Antenna Systems
Employment
Full-timeFrom the employer
Full-Time
Level
SeniorTeam
Engineering & Operations / E-Space USCountry assessment
Not doable from Austria because the employer's own board marks it as not remote.
Working conditions
Working hours: flexibility to occasionally work extended hours or weekends during critical periods is expected
Travel requirement: Some travel between sites may be required.
Our assessment is guidance. Confirm arrangements with the employer.
Job description
We are looking for a Senior Electromechanical Engineer to own electrical, optical and sensing harness/interconnect products for a space-based antenna application. This is a hands-on role for someone who enjoys developing unique solutions to unique problems - from preliminary system design and component selection to qualification, integration & flight.
What you'll do:
- Own the design and selection of the spacecraft’s wiring harness — electrical wiring, optical fiber, connectors, and interconnects.
- Own antenna specific sensors and their integration, routing, and signal interfaces.
- Define harness and connector requirements and drive component selection and supplier evaluation.
- Take harness, connectors, and fiber through qualification for the flight environment.
- Develop routing, strain-relief, and integration approaches compatible with a spacecraft structure.
- Create harness drawings, wire lists, and interface documentation.
- Support assembly, integration, and test, and resolve harness-related anomalies throughout the entire product lifecycle.
Required qualifications:
- Own the design and selection of the spacecraft’s wiring harness — electrical wiring, optical fiber, connectors, and interconnects.
- Own antenna specific sensors and their integration, routing, and signal interfaces.
- Define harness and connector requirements and drive component selection and supplier evaluation.
- Take harness, connectors, and fiber through qualification for the flight environment.
- Develop routing, strain-relief, and integration approaches compatible with a spacecraft structure.
- Create harness drawings, wire lists, and interface documentation.
- Support assembly, integration, and test, and resolve harness-related anomalies throughout the entire product lifecycle.
Preferred qualifications:
- Optical fiber / fiber-optic harness experience.
- Sensors and instrumentation integration.
- Space or flight environmental qualification (thermal-vacuum, vibration, radiation).
- Experience with space structures.
Location
On-site in California or Texas. Some travel between sites may be required.