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ePropelled The Future of
Electric Propulsion
Intelligent Power System - iPS500
Aircraft electronics continue to evolve as mission profiles become more
challenging and demanding. Longer flights and heavier payloads are
driving system designers to new heights. New levels of both energy and
system-level efficiencies are required to meet tomorrow’s aviation needs.
The 500-Watt ePropelled Intelligent Power Systems are a complete power
management solution for your aircraft. They provide steady regulated DC
power for your on-board avionics, servo and payload requirements. These
smart power systems also provide a wide array of real-time performance
and operational data for a range of useful applications and analytics.
ePropelled’s iPS500 provides complete power solutions for aviation applications.
The iPS500 takes in 3-phase sinusoidal AC voltages from starter generators like the
ePropelled SG500 and converts them to DC voltages to power on-board avionics,
servos and payloads. Input AC voltages will vary by the RPM of the Starter Generator or
Alternator and using active rectification and switching regulation the iPS500 will supply
the required DC output voltages.
Telemetry data for use with analytics, machine learning and artificial intelligence has
become a critical component to operational success of any air mission. The iPS500
monitors every input and output’s voltage and current level and provides the data
collected via an integrated Controller Area Network (CAN) interface. Aircraft and
power system designers can create custom applications via our open API (Application
Programming Interface) and you can set thresholds for alerts and alarms based on your
specific applications and mission profiles.
The Electronic Engine Starter (EES) feature can be used to drive the starter generator
during the engine start sequence. Once the engine is up to speed, the iPMC delivers
the regulated voltages. If for any reason the starter generator stops working, a backup
battery (if connected) automatically comes online and provides the voltages for a limited
duration depending on the backup battery size.
Fly Smarter
Intelligent Power Systems
ePropelled The Future of
Electric Propulsion
•	 One primary and up to two secondary outputs (12V & 5V)
•	 High efficiencies of up to 93.5%, (load dependent)
•	 Status reporting via software API and CAN Bus
•	 Software and hardware alerts to system controller
•	 Over-current limiting through voltage fold back
•	 Charges backup battery
•	 Configure various EES parameters for different IC engines
•	 	 Real time data monitoring for all voltages
•	 	 LED indicators provide status for each output voltage and current
•	 Aircraft Power Systems
•	 Unmanned Vehicle power systems
•	 Power conditioning in ground, maritime and aerospace applications
•	 Stand-alone power systems (SAPS) for remote area power supply
•	 Voltage regulation in the renewable power generation system
The figure below depicts the overall dimensions of the iPS Chassis. The four holes
marked with crosshairs are used for mounting the unit. Note: weight and other details
are given in the Technical Specification Table.
iPS500 Main Features
Mounting Instructions
Recommended Applications
iPS500 Technical Specifications
ePropelled The Future of
Electric Propulsion
iPS500 Rev 1.0 Specifications
INPUT
Parameter Min Max Notes
Input Voltage Range 25V 85V Vac RMS Line-to-Line. Frequency 3kHz max.
Maximum Total Input Power 545W at 50°C Ambient [122°F]
Maximum Total Input Power 667W at 40°C Ambient [104°F]
Maximum Back-up Battery Voltage 25.6V DC
Engine Starter Voltage Range 20V 33V DC (24V default)
Engine Starter Current Range 0A 20A At 24V DC, Open Loop 40A Peak/Phase
Start Trigger Voltage 2.3V 5V
Start Duration 1s 10s 20 Seconds between attempts
OUTPUT
Parameter Min Max Notes
Maximum Total Output Power (Continuous) 500W DC at 50°C Ambient [122°F]
Maximum Total Output Power (Continuous) 600W DC at 40°C Ambient [104°F]
Primary Output Voltage 28V DC (500W, 18A)
Secondary Output Voltage 1 12V DC (144W, 12A)
Secondary Output Voltage 2 5V DC (50W, 10A)
Voltage Regulation ±500mV
Voltage Ripple P-P <500mV
Peak Efficiency 93.5% At 60% full load
Protection Input under-voltage warning.
Output over-voltage warning.
Output short-circuit protection.
Output over-current protection.
Over temperature warning.
Backup Battery Switch Over.
MECHANICAL
Parameter Notes
Dimensions 7.95” x 3.73” x 2.13” [201.9mm x 94.7mm x 54.0mm]
Weight 1.60 pounds [724g]
Cooling Fan cooled
Ambient Operating Temperature -32°C to 50°C at 500W [-26°F to 122°F]
Storage Temperature -40°C to 85°C [-40°F to 185°F]
Ingress Protection IP20
ePropelled info@ePropelled.com
www.ePropelled.com
All specifications subject to change without notice. For more information, including ordering product, please contact
us at info@ePropelled.com. iPS500-1 rev062420
© 2020 by ePropelled
Pinouts
CONEC 3008W8SXX44A10X
Pin Label
A1 NOT USED
A2 VBAT+
A3 GND
A4 U-LEG
A5 V-LEG
A6 W-LEG
A7 -VSTART (RET)
A8 +VSTART
CONEC 3H15W4PAM99A10X
Pin Label
A1 +12V
A2 GND
A3 +28V
A4 GND
1-2 +5V
3-4 GND
5 STARTER ENABLE*
6 START, INPUT
7 BB SIGNAL, OUTPUT
8 GND
9 BAT 10K NTC
10 CAN+
11 CAN-
*NOTE: ”Starter enable” signal is used to
trigger the starter.
Assembled in USA
Warnings and Labels

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Fly Smarter - Intelligent Power System & Starter Generators from ePropelled

  • 1. ePropelled The Future of Electric Propulsion Intelligent Power System - iPS500 Aircraft electronics continue to evolve as mission profiles become more challenging and demanding. Longer flights and heavier payloads are driving system designers to new heights. New levels of both energy and system-level efficiencies are required to meet tomorrow’s aviation needs. The 500-Watt ePropelled Intelligent Power Systems are a complete power management solution for your aircraft. They provide steady regulated DC power for your on-board avionics, servo and payload requirements. These smart power systems also provide a wide array of real-time performance and operational data for a range of useful applications and analytics. ePropelled’s iPS500 provides complete power solutions for aviation applications. The iPS500 takes in 3-phase sinusoidal AC voltages from starter generators like the ePropelled SG500 and converts them to DC voltages to power on-board avionics, servos and payloads. Input AC voltages will vary by the RPM of the Starter Generator or Alternator and using active rectification and switching regulation the iPS500 will supply the required DC output voltages. Telemetry data for use with analytics, machine learning and artificial intelligence has become a critical component to operational success of any air mission. The iPS500 monitors every input and output’s voltage and current level and provides the data collected via an integrated Controller Area Network (CAN) interface. Aircraft and power system designers can create custom applications via our open API (Application Programming Interface) and you can set thresholds for alerts and alarms based on your specific applications and mission profiles. The Electronic Engine Starter (EES) feature can be used to drive the starter generator during the engine start sequence. Once the engine is up to speed, the iPMC delivers the regulated voltages. If for any reason the starter generator stops working, a backup battery (if connected) automatically comes online and provides the voltages for a limited duration depending on the backup battery size. Fly Smarter Intelligent Power Systems
  • 2. ePropelled The Future of Electric Propulsion • One primary and up to two secondary outputs (12V & 5V) • High efficiencies of up to 93.5%, (load dependent) • Status reporting via software API and CAN Bus • Software and hardware alerts to system controller • Over-current limiting through voltage fold back • Charges backup battery • Configure various EES parameters for different IC engines • Real time data monitoring for all voltages • LED indicators provide status for each output voltage and current • Aircraft Power Systems • Unmanned Vehicle power systems • Power conditioning in ground, maritime and aerospace applications • Stand-alone power systems (SAPS) for remote area power supply • Voltage regulation in the renewable power generation system The figure below depicts the overall dimensions of the iPS Chassis. The four holes marked with crosshairs are used for mounting the unit. Note: weight and other details are given in the Technical Specification Table. iPS500 Main Features Mounting Instructions Recommended Applications
  • 3. iPS500 Technical Specifications ePropelled The Future of Electric Propulsion iPS500 Rev 1.0 Specifications INPUT Parameter Min Max Notes Input Voltage Range 25V 85V Vac RMS Line-to-Line. Frequency 3kHz max. Maximum Total Input Power 545W at 50°C Ambient [122°F] Maximum Total Input Power 667W at 40°C Ambient [104°F] Maximum Back-up Battery Voltage 25.6V DC Engine Starter Voltage Range 20V 33V DC (24V default) Engine Starter Current Range 0A 20A At 24V DC, Open Loop 40A Peak/Phase Start Trigger Voltage 2.3V 5V Start Duration 1s 10s 20 Seconds between attempts OUTPUT Parameter Min Max Notes Maximum Total Output Power (Continuous) 500W DC at 50°C Ambient [122°F] Maximum Total Output Power (Continuous) 600W DC at 40°C Ambient [104°F] Primary Output Voltage 28V DC (500W, 18A) Secondary Output Voltage 1 12V DC (144W, 12A) Secondary Output Voltage 2 5V DC (50W, 10A) Voltage Regulation ±500mV Voltage Ripple P-P <500mV Peak Efficiency 93.5% At 60% full load Protection Input under-voltage warning. Output over-voltage warning. Output short-circuit protection. Output over-current protection. Over temperature warning. Backup Battery Switch Over. MECHANICAL Parameter Notes Dimensions 7.95” x 3.73” x 2.13” [201.9mm x 94.7mm x 54.0mm] Weight 1.60 pounds [724g] Cooling Fan cooled Ambient Operating Temperature -32°C to 50°C at 500W [-26°F to 122°F] Storage Temperature -40°C to 85°C [-40°F to 185°F] Ingress Protection IP20
  • 4. ePropelled info@ePropelled.com www.ePropelled.com All specifications subject to change without notice. For more information, including ordering product, please contact us at info@ePropelled.com. iPS500-1 rev062420 © 2020 by ePropelled Pinouts CONEC 3008W8SXX44A10X Pin Label A1 NOT USED A2 VBAT+ A3 GND A4 U-LEG A5 V-LEG A6 W-LEG A7 -VSTART (RET) A8 +VSTART CONEC 3H15W4PAM99A10X Pin Label A1 +12V A2 GND A3 +28V A4 GND 1-2 +5V 3-4 GND 5 STARTER ENABLE* 6 START, INPUT 7 BB SIGNAL, OUTPUT 8 GND 9 BAT 10K NTC 10 CAN+ 11 CAN- *NOTE: ”Starter enable” signal is used to trigger the starter. Assembled in USA Warnings and Labels