HARDWARE / PRODUCTAdded 24 Jul 2026

Modular Electrical Power System (IMEPS2)

Innovative Space Logistics
Modular Electrical Power System (IMEPS2)

The IMEPS2 is a second-generation modular electrical power system designed for small satellites, offering adaptable power solutions with superior efficiency and scalable redundancy.

Typed specifications139 values

Discloses 12 of 14 fields engineers filter by in this category (category median 7).

Mass
252 g
PBP-4S1P battery pack · datasheet p.8 48.7 g PBU  |  58 g PCU  |  57.4 g PDU (incl. bottom mount full CSKB)  |  51.6 g PDU (incl. top mount full CSKB)  +2
Total output power
48 W
max · PBU max output power per battery channel/pack at 12 V · datasheet p.9 64 W max · PBU max output power per battery channel/pack at 16 V
Envelope (L×W×H)
Height: PDU 11 mm, PBU 10 mm, PCU 12 mm, PBP-4S1P 21 mm
datasheet p.7 11 mm PDU Height
Outputs (as printed)
VD0: fixed (= rail voltage); VD1: user selectable (only below rail voltage); VD2: user selectable (only below rail voltage)
datasheet p.7 VDx: x 4 (Option using DaughterBoard mounted regulator)
Supply voltage
12.8 V
nom. · VD0 voltage domain (battery) · datasheet p.4 12.8 V Battery pack operating voltage  |  16 V PCU Output Voltage  |  3.3 V VD1 and VD2 voltage domain  |  12 V max · VD1 and VD2 voltage domain (custom)  +5
Power consumption
19.2 W
BU max input power (per battery channel/pack) at 12V · datasheet p.9 25.6 W BU max input power (per battery channel/pack) at 16V  |  48 W BU max output power (per battery channel/pack) at 12V  |  64 W BU max output power (per battery channel/pack) at 16V  |  0.063 W PBU idle consumption (3.9 mA at 16 V)  +8
Data interface
I2C
datasheet p.8 SPI optional  |  I2C two independent I2C interfaces; isolated I2C bus segment per …  |  UART  |  SPI optional  +2
Operating temperature
-40–70 °C
datasheet p.7 -40–70 °C operational temperature
Unit type
integrated EPS with battery
modular stack: PCU + PBU + PBP battery packs + PDU · datasheet p.4
Board format
CubeSat Kit bus
CSKB outputs and inter-stack CSKB connections · datasheet p.5 PC/104 follows a PC104 form factor  |  PC/104 PDU
Bus and outputs type
hybrid (regulated rails + battery bus)
VD0 = unregulated rail (battery) voltage; VD1/VD2 regulated b… · datasheet p.7
Unregulated (battery) bus voltage
12.8 V
PBP operating voltage · datasheet p.4 12.8 V PDU output channel Vbat  |  12.8–16 V common power rail voltage  |  16 V PBP operating voltage  |  16 V PDU output channel Vbat
Regulated output voltages
16 V
PCU output voltage (other voltages upon request) · datasheet p.4 12.8 V PDU VD0  |  3.3 V PDU VD1, VD2  |  12 V PDU_DB VDx  |  5 V VD1 default configuration  +5
Switchable outputs
4
PDU VD0 · datasheet p.4 4 PDU VD1  |  4 PDU VD2  |  4 PDU_DB  |  12 per PDU: VD0 x4, VD1 x4, VD2 x4 switchable channels
Solar array inputs
4
per PCU board: 4x MPPT channels · datasheet p.4
Solar input voltage window
2V min, 13V max
datasheet p.10 2 V min · PV input  |  13 V max · PV input with battery voltage >14V  |  2–13 V PV input min/max voltage (with battery voltage above 14 V)
Max solar input power
39 W
PCU per channel (5 series, 6 parallel solar cell strings) · datasheet p.4 39 W max · CU max input power per channel (5 series, 6 parallel solar ce…
Solar array regulation
MPPT
harvesting mechanism: Maximum Power Point Tracking; boost-onl… · datasheet p.9
Integrated battery energy
90 Wh
available configuration · datasheet p.2 45 Wh per PBP-4S1P pack (4 cells)  |  135 Wh available configuration
Protections
- Overcurrent/thermal limit on Unit input; - Overvoltage protection on all domains; - On each output bus channel: Overcurrent/thermal protection; - Voltage ramp slew rate control; - Reverse current protection; - Safety Mode (when VD0 low); - Emergency Low
datasheet p.8 watchdog hardware supervisor including watchdog; TT&C watchdog  |  over-current (LCL) overcurrent/thermal limit on unit input and on each output bu…  |  over-temperature overcurrent/thermal protection  |  over-voltage overvoltage protection on all domains; TVS diodes  +7
Connector
Harness interconnect: multicore wire, Harwin M80 L-Tek; daisy chain or point to point board interconnect
datasheet p.7
Survival temperature
-40–85 °C
datasheet p.7 -40–85 °C storage temperature
Flight heritage
Design based on heritage from ICEPS1 design flown on PEASSS CubeSat (2016). IMEPS1, first generation, flown in 2018. IMEPS2 first flown in 2020.
datasheet p.3
Satellite class
CubeSat
compliant to CubeSat standard; CubeSat missions from 3U upwards · datasheet p.1 nanosat 1-10 kg targeting larger nano- and micro-satellites from 3U upwards  |  microsat 10-100 kg targeting larger nano- and micro-satellites from 3U upwards
Missions flown
1
IMEPS1 · datasheet p.3 1 IMEPS2
Quasi-static load
10.8 g
design qualification load, static, three axes · datasheet p.3
Max current per output
3 A
PCU Maximum Input Current per channel · datasheet p.4 3 A PDU Max current per output channel (hardware current limited)  |  4 A PDU Max total current for VD1 (continuous)  |  6 A PDU Max total current for VD1 (peak)  |  4 A PDU Max total current for VD2 (continuous)  +15
Battery voltage range accepted
14.4 V
nom. · battery pack nominal voltage · datasheet p.8 12.8–16 V  |  16.8 V abs max, Battery pack abs max voltage  |  10 V min · Battery pack min voltage  |  12.8 V min · Common Power Rail  +3
Max battery charge current
1.6 A
Battery pack max input current · datasheet p.9 1.6 A max · battery pack max input current
MPPT
yes
hardware-based maximum power point tracking · datasheet p.2
Max solar input current
3 A
max · maximum input current per PCU channel · datasheet p.10
Integrated battery cell configuration
4 cells in series (PBP-4S1P), up to three battery packs per battery unit board
datasheet p.8
Battery heater control
yes
battery heating per pack, closed loop controlled, in orbit co… · datasheet p.9
Housekeeping telemetry
MCU/PCB temperature; voltage, current and power measurements on total unit input, total output for VD0/VD1/VD2 and each output bus channel; per cell voltage and 2x temperature sensors per battery pack
datasheet p.8
Redundancy
other
multiple PDU / PCU / PBU boards in parallel for redundancy; t… · 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 supplier20 lines, in the manufacturer's own wording
Flight heritage
since 2020
Battery packs
Up to 45 Wh per PBP, stackable for redundancy
Operating temperature
-40 to +70 °C
Storage temperature
-40 to +85 °C
Lifetime
12 months
Supply voltage
12.8 – 16.0 V
PDU Height
11 mm
PDU Mass
51.6 g (incl. top mount full CSKB)
PDU Idle consumption
66 mW (4.1 mA @ 16 V)
PDU Input maximum current
8 A
PDU Output maximum current
3 A per channel
PDU Total output maximum current (VD1)
4 A (continuous), 6 A(peak)
PDU Total output maximum current (VD2)
4 A (continuous), 6 A(peak)
Interface
I2C, UART, SPI optional
PBP Height
21 mm
PBP Mass
252 g
PBP Battery pack nominal voltage
14.4 V
PBP Battery pack operating voltage
12.8-16.0 V
PBP Battery pack nominal capacity
3200 mAh
PBU Height
10 mm

About

The second-generation Modular Electrical Power System (IMEPS2) redefines Electrical Power Subsystems for small satellites. Built on a modular, distributed design, it enables unmatched adaptability, tailoring power solutions to your platform’s exact needs without full customization. With cutting-edge technology, IMEPS2 ensures superior efficiency, reduced EMI, and scalable redundancy across. It features battery packs that expand storage with up to 45Wh per PBP, which are stackable for redundancy. The system also includes power conditioning with scalable MPPT channels for optimal solar input, and power distribution with fully configurable outputs and time delays, user-defined voltages, and robust redundancy options for mission assurance. It has flight heritage since 2020.

Documentation

Need the full ICD, test reports or a specific revision? Ask the supplier directly.

Source: www.isispace.nl ↗

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