Daniel Johnson Email & Phone Number

• Perform thermal vacuum pressure testing of Orbital Replacement Units (ORUs) for the International Space Station, from -80°C to +150°C and as low as 10-8 Torr or 1.3µ pascals. Test boxes and cables for test equipment.

• Perform thermal vacuum pressure testing of Orbital Replacement Units (ORUs) for the International Space Station, from -80°C to +150°C and as low as 10-8 Torr or 1.3µ pascals. Test boxes and cables for test equipment.
• Procure complex hardware, assemble product prototypes (including modification of existing hardware) and tested IR&D Capacitive Couple Charge Pump power supply. Testing include designing Lab View Applications, powering.
• Procure complex hardware, assemble product prototypes (including modification of existing hardware) and tested IR&D Capacitive Couple Charge Pump power supply. Testing include designing Lab View Applications, powering.

• Acquired $50,000 of IR&D money to design and develop Dual Series Boost Regulator Power Management and Distribution System for laboratory test configuration of a Solar Array system. Procured hardware, created assembly.
• Responsible for procurement, assembly and creation… Show more
• Responsible for procurement, assembly and creation of Engineering Product Development documents for the Orion Portable Equipment Panel (PEP). Utilized space hardened avionic hardware to create engineering product parts.
• Performed Lean Six Sigma analysis of data collected at the process level of complaints by the design engineering team. Created pareto, histograms and scatter charts of data and assigned priority to design team.

Canoga Park, CA

• Designed, acquired hardware, created product development instructions and assembled complex product prototype of the J-2X Engine Controller (EC) Backplane including testing and creation of Embedded Software Design.
• Performed worst case circuit analysis and created Engineering Product… Show more
• Performed worst case circuit analysis and created Engineering Product Development documents for the J-2X Spark Exciter. The Spark Exciter is part of the J-2X rocket engine ignition system that utilized an inductor and.
• Performed worst case circuit analysis and created Engineering Product Development documents for the Speed Sensor Signal Conditioner including design of Embedded Software. The Speed Sensor Signal Conditioner provides.
• Responsible for design and development of the Multiple Kill Vehicle (MKV) Test System Software GUI. The MKV Test Systems GUI interfaced with Reflective memory and an Ethernet bus while utilizing User Datagram Protocol.
• Responsible for the maintenance and delivery of Kinetic Weapon Control Systems to customers in Maryland’s Johns Hopkins University ( Applied Physics Lab), White Sands Missile Range (New Mexico), Boeing (Anaheim.

Canoga Park, CA

• Maintained and tested Orbital Replacement Units (ORUs) that supported the International Space Station Freedom power system.
• Developed effective assembly and test sequences from engineering drawings and work instructions to ensure program schedules were met.

• Maintained and tested Orbital Replacement Units (ORUs) that supported the International Space Station Freedom power system.
• Developed effective assembly and test sequences from engineering drawings and work instructions to ensure program schedules were met.

Electronic Engineering

Bachelor Of Science, Electrical And Computer Engineering

Activities and Societies: Jazz Band