HARDWARE / PRODUCTUpdated 31 Aug 2026

Electrical Power System

Dragonfly Aerospace
Electrical Power System

Dragonfly’s advanced 28V Electrical Power System designed for spacecraft power control and distribution, now in its 8th generation with heritage design for exceptional reliability and performance.

Typed specifications65 values

Discloses 9 of 14 fields engineers filter by in this category (category median 7).

Mass
3 300 g
datasheet p.1 3 300 g 1x SRM-S3R-18-LP & 3x PDM-LP-752 configuration
Total output power
1 500 W
PDM-HP-50 module total output power · datasheet p.1 600 W PDM-LP-752 module total output power  |  60 W PDM-REG module total output power  |  1 500 W Total Input, Output & Battery Power
Envelope (L×W×H)
211 x 153 x 175 mm
datasheet p.1 211 x 153 x 175 mm 1x SRM-S3R-18-LP & 3x PDM-LP-752 configuration
Outputs (as printed)
Unregulated unprotected power bus port & PDM ports as per configuration options
datasheet p.1
Supply voltage
29.7 V
nom. · datasheet p.1 22 V min  |  32 V max  |  22–32 V Centralised (EPS Housing)
Power consumption
1 500 W
product page 600 W  |  1 500 W
Data interface
CAN
datasheet p.1
Operating temperature
-10 °C
min · datasheet p.1 50 °C max  |  -10–50 °C
Radiation tolerance (TID)
20 krad
datasheet p.1 20 krad screening
Design lifetime
8 years
LEO · datasheet p.1 8 years max · LEO
TRL
9
datasheet p.1
Export status
ITAR-free
datasheet p.1
Unit type
PCDU
spacecraft power control, distribution and protection system · datasheet p.1
Bus and outputs type
hybrid (regulated rails + battery bus)
unregulated 29.7 V bus + PDM-REG 5 V regulated · datasheet p.1
Unregulated (battery) bus voltage
29.7 V
nom. · bus voltage · datasheet p.1 29.7 V Centralised (EPS Housing)  |  29.7 V unregulated  |  22–32 V bus voltage
Regulated output voltages
5 V
PDM-REG regulated output · datasheet p.1
Switchable outputs
2
PDM-HP-50 output channels · datasheet p.1 8 PDM-LP-752 output channels  |  8 PDM-REG output channels
Solar input voltage window
22 V
min · datasheet p.1 32 V max
Max solar input power
535 W
1 x SRM total input power at 29.7 V · datasheet p.1
Solar array regulation
S3R (sequential switching shunt)
SRM topology: S3R (Sequential Switching Shunt Regulator) · datasheet p.1
Protections
Over current
datasheet p.1 under-voltage lockout battery under voltage protection (hibernation)  |  over-current (LCL) over current, all distribution channels  |  other over load  |  watchdog watchdog timer function (1 hr to 72 hrs)  +3
Flight heritage
TRL 9
datasheet p.1
Max current per output
50 A
PDM-HP-50, 2 channels · datasheet p.1 50 A PDM-HP-50, 2x 50 A channels  |  7 A PDM-LP-752, 1 channel  |  7 A PDM-LP-752, 1x 7 A channel  |  5 A PDM-LP-752, 2 channels  +7
MPPT
no
datasheet p.1
Max solar input current
18 A
max · 1 x SRM · datasheet p.1
Housekeeping telemetry
Telemetry & Telecommands over CAN
datasheet p.1
Redundancy
other
Dual Redundant; single fault tolerance · datasheet p.1

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 supplier12 lines, in the manufacturer's own wording
Total input, output & battery power
1500 W
Supply voltage
29.7 V (22 - 32 V)
Communication interfaces
CAN Telemetry & Telecommands, DCL (Direct Command Line) Telecommands
Operating temperature
-10 °C to +50 °C
Dimensions
211 x 153 x 175 mm
Mass
3.3 kg
Design life
Up to 8 years LEO (20 kRad screening)
Srm total input power
535 W at 29.7 V (18 A max)
Pdm-lp-752 total output power
600 W
Pdm-lp-752 no. of output channels
8
Pdm-hp-50 total output power
1500 W
Pdm-hp-50 no. of output channels
2

About

The EPS-LP-1k5 is Dragonfly’s advanced 28V Electrical Power System, specifically designed for spacecraft power control and distribution. This system, now in its 8th generation, boasts a heritage design that ensures exceptional reliability and performance, making it an ideal solution for nano, micro, and mini satellites. It offers up to 1500 W total power and features a centralized configuration within the EPS Housing. Key functionalities include a Spacecraft Power Cycle Watchdog Timer Function (1 hr to 72 hrs), single fault tolerance, Battery Under Voltage Protection (Hibernation), and Battery Charge Current Limiting. The system also incorporates a Solar Regulator Module (SRM) with S3R (Sequential Switching Shunt Regulator) topology, providing 535 W total input power at 29.7 V. Distribution channels are protected with overcurrent, overload, and external trip input, along with watchdog timers and auto-retry redundancy. The EPS-LP-1k5 is ITAR-Free and has a TRL 9 rating.

Documentation

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

Source: dragonflyaerospace.com ↗

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