Our purpose is to offer a viable airborne power solution alternative that meets the primary need to be in compliance with aeronautics specification RTCA/DO-160D/E, Boeing's D6-44588 and Airbus’s ABD0100.1.8 specifications.

Benefits of our Conventional Design Approach:

• Lower cost NRE to develop a customized power supply
• Shortens lead-time for prototype sample delivery
• Reduces the risk associated with the creation of a new design and the production development

Aircraft Power Supply
Compliance Design Parameters:

• RTCA/DO-160D for conducted emissions, power input and susceptibility requirements (Section 21, 16 & 18)
• Airbus ABD0100.1.8 issue D for power factor and input current harmonic
• Wide frequency operating range (360Hz -800Hz)
• Extended Holdup Time

1500 Watts
Single Output Power Supply:

• Airborne Military Power Supplies.
• Airborne Commercial Power Supplies (DO-160)
• MIL-STD Ship Board Power Supplies.
• MIL-STD Land Based Power Supplies
• Industrial Standard Power Supplies (not MIL-STD)