PPU-1500 (Power Processing Unit)
Space Electric Thruster Systems (SETS)
The PPU-1500 is a power processing unit for 1.5 kW class electric propulsion systems, designed to convert satellite power and control thruster operations.
Typed specifications18 values
Discloses 4 of 8 fields engineers filter by in this category (category median 2).
- Propulsion family
- electric power processing unit for electric propulsion systems in the … · datasheet p.1
- Supply voltage
- 80–140 V Input Voltage · datasheet p.2 80–140 V inverter input voltage
- Power consumption
- 800–1 500 W product page
- Data interface
- CAN Communication · datasheet p.2 MIL-STD-1553 MIL-1553B (optional) | Ethernet optional | MIL-1553B optional, Communication | RS-485 Communication +1
- Operating temperature
- -35–80 °C product page
- Radiation tolerance (TID)
- 30 krad Radiation tolerance (COTS) · datasheet p.2 30 krad max · COTS
- TRL
- 4 datasheet p.2
- Power at thrust
- 800–1 500 W Discharge Power, Anode Power Supply · datasheet p.2
- PPU output power
- 1 500 W max · Discharge Power · datasheet p.2 800–1 500 W discharge power
- Discharge (anode) voltage
- 200–500 V datasheet p.2
Each value is typed with its unit and measurement condition and cites the datasheet page it was taken from. Nothing is guessed: a field that is absent here has not been published by the manufacturer. machine-extracted ✓ checked by NewSpace Market ✓ manufacturer confirmed by the manufacturer.
As published by the supplier14 lines, in the manufacturer's own wording
- Anode power
- Up to 1500 W
- Supply voltage
- 80-140 V
- Operating temperature
- -35 to +80 C
- Efficiency
- Up to 94%
- Input Voltage
- 80 – 140 VDC
- Data Interface
- CAN, RS-485, MIL-1553B (optional), Ethernet (optional)
- Discharge Power
- 800 – 1500 W
- Discharge Voltage
- 200 – 500 VDC
- Ignition Voltage
- 400 VDC
- Valves Number
- Up to 9
- Actuation Voltage
- 28 VDC
- Holding Voltage
- 7 VDC
- Radiation tolerance (COTS)
- Up to 30 kRad
- TRL
- 4
About
The PPU-1500 is a power processing unit (PPU) engineered for electric propulsion systems in the 1.5 kW class. Its primary function is to convert onboard satellite power and precisely control the operation of electric propulsion subsystems, including Hall thrusters like the ST-100 and the Xenon Feed System. A laboratory model of the PPU-1500 has undergone testing with Hall thrusters up to 1.5 kW under laboratory conditions, demonstrating strong performance. An engineering model is currently under development with the goal of validating the system for flight applications. The PPU-1500’s architecture is designed with flexibility and future missions in mind, incorporating the capability to transition to radiation-hardened components without requiring a complete redesign. This design approach makes the PPU-1500 suitable for a broad spectrum of missions, ranging from Low Earth Orbit (LEO) to more demanding environments such as Medium Earth Orbit (MEO), Geostationary Earth Orbit (GEO), and deep space.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.