Custom PMDSAS Panel, Body-Mounted, per Cell
Custom body-mounted solar panels built with Pumpkin's Modular Deployable Solar Array System (PMDSAS) technology, priced per solar cell, with a 100% on-orbit success rate since 2008.
Typed specifications43 values
Discloses 7 of 12 fields engineers filter by in this category (category median 3).
- Output power (BOL)
- 1 W nom. · nominal power BOL, AM0, 1 XTJ Prime cells, 1S1P (approximate) · datasheet p.17 12 W nom. · nominal power BOL, AM0, 12 XTJ Prime cells, 12S1P (approximate) | 2 W nom. · nominal power BOL, AM0, 2 XTJ Prime cells, 2S1P (approximate) | 24 W nom. · nominal power BOL, AM0, 24 XTJ Prime cells, 12S2P (approximate) | 3 W nom. · nominal power BOL, AM0, 3 XTJ Prime cells, 3S1P (approximate) +5
- Cell efficiency
- 30.7 % Spectrolab XTJ Prime · datasheet p.4
- Deployable
- no fixed / body-mounted panel · datasheet p.5
- Array configuration
- body-mounted panel custom fixed (body-mounted) PMDSAS panel; document also cover… · datasheet p.5
- Cell type
- triple-junction GaAs Spectrolab NeXt Triple Junction (XTJ) Prime (standard); other… · datasheet p.4
- Cell part number
- Spectrolab CIC 30.7% NeXt Triple Junction (XTJ) Prime datasheet p.4
- Open-circuit voltage at the panel output (Voc)
- 2.5 V approximate string voltage, 1 XTJ Prime cells, 1S1P · datasheet p.17 30 V approximate string voltage, 12 XTJ Prime cells, 12S1P | 5 V approximate string voltage, 2 XTJ Prime cells, 2S1P | 30 V approximate string voltage, 24 XTJ Prime cells, 12S2P | 7.5 V approximate string voltage, 3 XTJ Prime cells, 3S1P +6
- Number of strings
- 1 typical CubeSat-class panel: all cells in a single string (NS… · datasheet p.17
- Integrated devices
- other blocking Schottky diodes (at least two per string); bleed res… · datasheet p.16 bypass diodes integral back diode in each CIC | temperature sensor LM335A analog or customer-specified | coarse sun sensor photodiode for coarse sun sensors (optional component)
- Connector
- Harness connector Hirose DF13 series (POS, RTN and telemetry); standard fixed panels: 6-pin Hirose harness datasheet p.16
- Flight heritage
- 600+ panels flown since 2008, 100% on-orbit success rate, LEO to GTO product page
- Satellite class
- CubeSat CubeSat-compatible solar panels · datasheet p.4 nanosat 1-10 kg fixed and deployable solar panels for nanosatellites
- Short-circuit current (Isc)
- 0.4 A ca. 400mA per XTJ Prime CIC (printed per cell) · datasheet p.17
- Substrate
- FR4 PCB FR4, FR406 or similar; Rogers laminates possible on custom pa… · datasheet p.4
- Cell area
- 26.62 cm² Spectrolab XTJ Prime CIC · datasheet p.20
- Integrated sensors (as printed)
- Temperature sensor LM335A (analog output, absolute Kelvin, SO-8) or customer-specified; photodiode for coarse sun sensors datasheet p.16
- Panel thickness
- 0.79 mm nom. · COTS panels standard PCB thickness .031in; Pumpkin PRM compat… · datasheet p.4 0.79 mm min · standard panels .031in [0.79mm] to .062in [1.57mm] | 1.57 mm max · standard panels .031in [0.79mm] to .062in [1.57mm]; other thi…
- Bypass diodes
- per cell each CIC includes an integral back diode · datasheet p.17
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 supplier8 lines, in the manufacturer's own wording
- Technology
- Pumpkin Modular Deployable Solar Array System (PMDSAS)
- Mounting type
- Body-mounted
- On-orbit heritage
- 600+ panels flown since 2008, 100% on-orbit success rate, LEO to GTO
- Solar cell efficiency (historical)
- ~28% AM0 (early triple-junction cells)
- Solar cell efficiency (current)
- >32% AM0
- Optional features
- Temperature sensors, PRM features, connectors, harnesses
- Testing
- Vacuum bakeout and comprehensive irradiance test performed on every panel
- Pricing basis
- Per solar cell (custom panel geometry)
About
This listing covers custom, body-mounted solar panels built using Pumpkin’s Modular Deployable Solar Array System (PMDSAS) technology and priced per individual solar cell. Since their debut in 2008, over 600 PMDSAS solar panels have flown with a 100% success rate on-orbit, spanning missions from LEO all the way to GTO. Pumpkin describes the panels as flight hardware, flight qualified, and space proven.
Customers can specify essentially any panel geometry, and Pumpkin will work to maximize available solar power while incorporating additional features such as temperature sensors, PRM (panel removal mechanism) features, connectors, and harnesses. Pumpkin’s proprietary PMDSAS construction methods are intended to produce an extremely robust panel able to withstand launch loads and vibration. Every panel undergoes a vacuum bakeout followed by a comprehensive irradiance test to verify proper operation before delivery.
Over the years, PMDSAS panels have migrated from triple-junction solar cells starting around 28% AM0 efficiency to cells now exceeding 32% AM0 efficiency, allowing higher power density on the same footprint. Because the panels are custom-configured, pricing on the storefront is per cell; the product page notes purchasing restrictions apply.
Documentation
Need the full ICD, test reports or a specific revision? Ask the supplier directly.