Electrical Engineer II

Client Growth Resources, Inc; Los Angeles (CA); On-site; USD 130,000 - 165,000; Full time

Benefits offered by this job

Benefits

Job summary

Client Growth Resources, Inc. is seeking an Electrical Engineer II in Los Angeles to own and advance spacecraft power systems, working with high-voltage hardware for space use.

The role requires 4+ years in spacecraft electrical engineering, a Bachelor's degree, and the ability to operate onsite in a high-technology manufacturing environment.

Qualifications

• Bachelor's degree required.

Responsibilities

• Own the electrical power subsystem (EPS/PCDU) for the spacecraft, including power generation, conditioning, distribution, and battery systems.
• Design high-voltage PMAD systems that run reliably in vacuum, accounting for plasma charging and corona discharge.
• Manage high-voltage battery state of health and ensure electrical components work together reliably.
• Take hardware from a smallsat demonstrator to flight using breadboarding, schematics, PCB layout, bench testing, and debugging.
• Guide electrical hardware through AI&T and environmental qualification.

Education

Bachelor's Degree

Job description

TITLE: Electrical Engineer II

ENVIRONMENT: Hardware, Manufacturing, Aerospace

LOCATION:Los Ángeles, CA Onsite

COMPENSATIONRANGE:$130,000.00 - $165,000.00 DOE

DEGREEREQUIREMENTS:Bachelors Degree

CITIZENSHIP: Must be a U.S. Citizen or Green Card Holder and able to work for any U.S. Employer

BENEFITPACKAGE: Yes

EXPERIENCELEVEL:4+ years experience

POSITIONSUMMARY:

We are looking for an Electrical Engineer II with 4+ years of experience in spacecraft electrical engineering to own the power systems behind our modular power plant in space. We will let satellites and spacecraft connect to it and draw power in orbit. We need a space-native engineer who is comfortable with very high voltage systems, battery state of health, and how electrical components work together in the space environment.

What will you be doing?

• Owning the electrical power subsystem (EPS/PCDU) for the spacecraft, including power generation, conditioning, distribution, and battery systems
• Designing high-voltage power management and distribution (PMAD) systems that run reliably in vacuum, accounting for plasma charging, magnetosphere interactions, corona discharge, and electrical breakdown
• Managing high-voltage battery state of health and making sure electrical components work together reliably across the spacecraft
• Taking hardware from a smallsat demonstrator to flight using breadboarding, schematics, PCB layout, bench testing, and debugging
• Guiding electrical hardware through Assembly, Integration & Test (AI&T) and environmental qualification

Tech stack

Altium, KiCad, SPICE, Schematic Capture, PCB Layout, EPS/PCDU, High-Voltage PMAD, DC-DC Conversion, Battery Management Systems, Solar Arrays, EMI/EMC Filtering, Thermal-Vacuum Testing, Radiation Design, AI&T