| 32% Efficiency Triple Junction GaAs Solar Cell |
CAVU Aerospace
|
0.0024 |
1.33 |
2.7 |
— |
— |
PDF
|
| TJ 3G30-Advanced Space Solar Cell (4x8) |
AZUR SPACE
|
0.0026 |
— |
— |
— |
— |
PDF
|
| QJ 4G32-Advanced Space Solar Cell (4x8) |
AZUR SPACE
|
0.0033 |
— |
— |
— |
— |
PDF
|
| 30% Efficiency Triple Junction GaAs Solar Cell |
CAVU Aerospace
|
0.0036 |
— |
0.9 |
80.2 |
30% at the beginning of life (BOL) under |
PDF
|
| nanoSSOC-D60 Digital Sun Sensor |
Solar MEMS Technologies
|
0.005 |
0.1 |
3.3–5 |
— |
— |
— |
| TJ 3G30-Advanced Space Solar Cell (8x8) |
AZUR SPACE
|
0.0052 |
— |
— |
— |
— |
PDF
|
| TJ 3G30-Advanced Space Solar Cell (6x12) |
AZUR SPACE
|
0.0061 |
— |
— |
— |
— |
PDF
|
| QJ 4G32-Advanced Space Solar Cell (8x8) |
AZUR SPACE
|
0.0065 |
— |
— |
— |
— |
PDF
|
| QJ 4G32-Advanced Space Solar Cell (HP) |
AZUR SPACE
|
0.01 |
— |
— |
— |
— |
PDF
|
| TJ 3G30-Advanced Space Solar Cell (HP) |
AZUR SPACE
|
0.01 |
— |
— |
— |
— |
PDF
|
| Redwire Rigid Panel Solar Array Systems |
Redwire Corporation
|
0.02 |
15000 |
— |
— |
— |
— |
| Power supply system (with battery unit) |
SPUTNIX
|
0.02 |
0.2 |
3.5–5.5 |
— |
— |
— |
| CubeSat GaAs Side Solar Panel SXC-SGS-03 |
SPUTNIX
|
0.03 |
— |
5–5.5 |
98 |
28% |
— |
| GaAs side solar panel with coils |
SPUTNIX
|
0.03 |
— |
5–5.5 |
98 |
28% |
— |
| Ra |
Spacemanic s.r.o.
|
0.03 |
1 |
— |
— |
> 30% |
PDF
|
| Unified DC-DC Conversion Module |
Glavkosmos
|
0.03 |
— |
12–50 |
— |
85% |
— |
| Unified Power Management and Control Module |
Glavkosmos
|
0.03 |
— |
4.5–5.5 |
— |
— |
— |
| SXC-SG-03 GaAs Solar Panels (Side / End) |
SPUTNIX
|
0.03 |
— |
5.3 |
98 |
28 |
— |
| Si Solar Panel with Coils (side) |
Glavkosmos
|
0.032 |
— |
5.4 |
98 |
— |
— |
| GaAs Solar Panel with Coils (end edge) |
Glavkosmos
|
0.032 |
— |
5.3 |
98 |
— |
— |
| Si Solar panel with Coils (end edge) |
Glavkosmos
|
0.032 |
— |
5.4 |
98 |
— |
— |
| GaAs Solar Panel with Coils (side) |
Glavkosmos
|
0.034 |
— |
5.4 |
98 |
28% |
— |
| CubeSat GaAs End/Edge Solar Panel SXC-SGE-03 |
SPUTNIX
|
0.037 |
— |
5–5.5 |
98 |
28% |
— |
| GaAs end edge solar panel with coils |
SPUTNIX
|
0.037 |
— |
5–5.5 |
98 |
28% |
— |
| SP1X |
NPC Spacemind
|
0.04 |
2.3 |
4.6–5 |
— |
— |
— |
| SP Body-Mounted Solar Panels |
NPC Spacemind
|
0.04 |
— |
— |
— |
— |
— |
| SP1Z |
NPC Spacemind
|
0.045 |
2.3 |
4.6–5 |
— |
— |
— |
| Satellite Solar Panels |
ISISPACE Group
|
0.05 |
1.23 |
2.7 |
— |
— |
— |
| Modular Electrical Power System 2 |
ISISPACE Group
|
0.058 |
39 |
8 |
— |
— |
PDF
|
| Power Supply System [with battery unit] |
Glavkosmos
|
0.058 |
0.16 |
3–6 |
96 |
— |
— |
| CubeSat EPS - STARBUCK-Nano |
AAC Clyde Space
|
0.086 |
— |
8.2 |
— |
— |
PDF
|
| SP2X |
NPC Spacemind
|
0.087 |
4.6 |
9.2–10 |
— |
— |
— |
| NART-EPS Electric Power Subsystem (EPS) |
Gumush
|
0.103 |
25 |
20 |
93 |
— |
— |
| VES16 Cell |
Saft
|
0.112 |
— |
2.7–4.1 |
— |
— |
— |
| ODALISS Solar Panels |
Emxys
|
0.123 |
66.6 |
14.7 |
327.5 |
higher than 29% |
PDF
|
| NEA® 8020 Series Battery Cell Bypass Switch |
Ensign-Bickford Aerospace & Defense (EBAD)
|
0.13 |
— |
— |
— |
— |
— |
| NEA® 8030 Series Battery Cell Bypass Switch |
Ensign-Bickford Aerospace & Defense (EBAD)
|
0.13 |
— |
— |
— |
— |
— |
| SP3X |
NPC Spacemind
|
0.137 |
8 |
16–17.5 |
— |
— |
— |
| E28-200 28V SmallSat Electric Power System |
ibeos
|
0.14 |
2.5 |
33.6 |
96 |
— |
— |
| E14-150 14V SmallSat Electric Power System |
ibeos
|
0.14 |
1.8 |
16.8 |
96 |
— |
— |
| 3U Solar Panel |
EnduroSat
|
0.147 |
8.4 |
17.5 |
— |
— |
— |
| STARBUCK-NANO CubeSat EPS |
AAC Clyde Space
|
0.148 |
— |
8.2 |
— |
— |
PDF
|
| Electrical Power System (EPS) 2000 |
C3S LLC
|
0.15 |
2000 |
6–70 |
— |
— |
PDF
|
| Compact Electrical Power System 2 |
ISISPACE Group
|
0.184 |
— |
0 |
— |
— |
PDF
|
| Amun |
Spacemanic s.r.o.
|
0.185 |
— |
7.2 |
95.9 |
— |
PDF
|
| IMT µSADA Miniaturized Solar Array Drive Assembly |
IMT (Ingegneria Marketing Technologies)
|
0.25 |
0.5 |
31–54 |
— |
— |
— |
| OPTIMUS Battery |
AAC Clyde Space
|
0.268 |
0.1 |
8.3 |
— |
— |
PDF
|
| PCDU — Power Conditioning and Distribution Unit |
Terma
|
0.27 |
15000 |
28–50 |
— |
— |
— |
| GEMINI EPS |
NPC Spacemind
|
0.3 |
— |
5–20 |
— |
— |
— |
| PHOTON CubeSat Solar Arrays |
AAC Clyde Space
|
0.33 |
3 |
— |
— |
— |
PDF
|
| SP6X |
NPC Spacemind
|
0.335 |
18.4 |
18.4–20 |
— |
— |
— |
| ODALISS PDCU |
Emxys
|
0.36 |
36 |
7.4 |
870 |
— |
PDF
|
| B14-M45/M90 14V Modular SmallSat Battery |
ibeos
|
0.375 |
8 |
13.2–16.8 |
94.5 |
— |
— |
| SP8X |
NPC Spacemind
|
0.45 |
23 |
23–25 |
— |
— |
— |
| High Capacity Batteries |
Blue Canyon Technologies
|
0.65 |
— |
— |
— |
— |
PDF
|
| 4S1P VES16 Battery |
Saft
|
0.7 |
— |
13.2–16.4 |
— |
— |
— |
| B28-135 28V SmallSat Battery |
ibeos
|
0.85 |
20 |
22–33.6 |
94.5 |
— |
— |
| Umbra Battery Module (8S1P/8S2P) |
Umbra Lab Inc.
|
0.93 |
— |
22–31 |
— |
— |
PDF
|
| PCU-110 |
Berlin Space Technologies
|
1.08 |
— |
23.1 |
186 |
— |
PDF
|
| High-power distribution and control unit |
SPUTNIX
|
1.1 |
— |
22–34 |
244 |
— |
— |
| Origami Solar Array |
Dcubed
|
1.2 |
100 |
14–28 |
— |
— |
— |
| Solar Array Mechanical Device |
Glavkosmos
|
1.5 |
25000 |
— |
— |
— |
— |
| ABSL CM170 4s6p Li-ion Space Battery (14 V, 12 Ah) |
EnerSys / ABSL Space Products
|
1.6 |
— |
12–16.8 |
132 |
— |
PDF
|
| Solar Panels |
Ananth Technologies
|
2 |
230 |
|
— |
Up to 31% |
— |
| ABSL CM230 8s4p Li-ion Space Battery (28 V, 8 Ah) |
EnerSys / ABSL Space Products
|
2.05 |
— |
24–33.6 |
168 |
— |
PDF
|
| B28-M275/550/825/1100 28V Modular Battery Series |
ibeos
|
2.1 |
— |
24–33.6 |
— |
— |
— |
| Voltage Converter Single-phase, Upgraded POS-80-RNM |
Glavkosmos
|
2.5 |
80 |
24–34 |
— |
85% |
— |
| B50-412/825/1237 50V Modular Battery Series |
ibeos
|
3 |
— |
36–50.4 |
— |
— |
— |
| BAT-110 |
Berlin Space Technologies
|
3 |
— |
23.1 |
240 |
— |
PDF
|
| SmallSat PCDU - STARBUCK-Mini MCC |
AAC Clyde Space
|
3.9 |
10 |
22–34 |
— |
— |
— |
| SmallSat PCDU - STARBUCK-MINI |
AAC Clyde Space
|
3.9 |
10 |
22–34 |
— |
— |
— |
| VPCDU-1 Power Control and Distribution Unit |
VECTRONIC Aerospace GmbH
|
4.14 |
360 |
22.5–60 |
220 |
— |
— |
| ABSL CM520 8s9p Li-ion Space Battery (28 V, 18 Ah) |
EnerSys / ABSL Space Products
|
4.3 |
— |
24–33.6 |
209 |
— |
PDF
|
| Solar Array Drive Mechanism. Type 4 |
Glavkosmos
|
4.3 |
— |
— |
260 |
— |
— |
| 135W Dual Articulated Deployable Solar Array |
Pumpkin, Inc.
|
4.36 |
135 |
— |
— |
— |
— |
| Solar Array Drive Mechanism. Type 6 |
Glavkosmos
|
4.6 |
— |
— |
290 |
— |
— |
| VES16 8S4P Battery |
Saft
|
5 |
— |
25–32.8 |
— |
— |
— |
| 220W Deployable Clamshell Solar Array (DCSA) |
Pumpkin, Inc.
|
5.05 |
220 |
20–40 |
— |
— |
PDF
|
| SADM-200 |
Comat
|
6.65 |
200 |
14 |
— |
— |
PDF
|
| Regulation and control equipment |
SPUTNIX
|
7 |
— |
22–34 |
306 |
— |
— |
| ABSL CM1040 36s4p Li-ion Space Battery (126 V, 8 Ah) |
EnerSys / ABSL Space Products
|
8.4 |
— |
108–151.2 |
362 |
— |
PDF
|
| ABSL CM1040 8s18p Li-ion Space Battery (28 V, 36 Ah) |
EnerSys / ABSL Space Products
|
8.8 |
— |
24–33.6 |
362 |
— |
PDF
|
| Regulation and Monitoring Equipment of Electric Power Supply System EPS) ARK-MKA |
Glavkosmos
|
12 |
700 |
32 |
— |
— |
— |
| Rechargeable Battery for Power Supply of Spacecraft and Ground Infrastructure |
Glavkosmos
|
14.5 |
— |
23.8 |
472 |
— |
— |
| Voltage Converter PN120/28 |
Glavkosmos
|
15.5 |
1500 |
110–180 |
340 |
92% |
— |
| Redwire HiPASS - High-Power Rigid Array Solution for SmallSats |
Redwire Corporation
|
17 |
— |
— |
— |
— |
PDF
|
| SmallSat EPS |
EnduroSat
|
19.5 |
— |
|
— |
— |
— |
| ABSL CM2300 16s20p Li-ion Space Battery (56 V, 40 Ah) |
EnerSys / ABSL Space Products
|
19.6 |
— |
48–67.2 |
359 |
— |
PDF
|
| ABSL CM2300 8s40p Li-ion Space Battery (28 V, 80 Ah) |
EnerSys / ABSL Space Products
|
20 |
— |
24–33.6 |
359 |
— |
PDF
|
| ST Engineering Power Control & Distribution Unit (PCDU) |
ST Engineering Satellite Systems
|
24.5 |
4000 |
22–38 |
— |
— |
PDF
|
| Voltage Converter PN28/120 |
Glavkosmos
|
25 |
2000 |
28.5 |
340 |
92% |
— |
| ARC Regulation and Control Equipment for Manned and Cargo Spacecraft |
Glavkosmos
|
26 |
2800 |
32 |
— |
— |
— |
| VES16 11S16P Battery |
Saft
|
28.8 |
— |
29.7–45.1 |
— |
— |
— |
| Roll Out Solar Array (ROSA) |
Redwire Corporation
|
36 |
3300 |
12 |
— |
— |
PDF
|
| Rechargeable Battery for Power Supply of Spacecraft |
Glavkosmos
|
74 |
— |
28.8 |
530 |
— |
— |
| High-capacity Rechargeable Battery for Power Supply of Spacecraft and Ground Infrastructure |
Glavkosmos
|
82 |
— |
27.6 |
619 |
— |
— |
| Rechargeable Battery for Power Supply of Ground Infrastructure |
Glavkosmos
|
115 |
— |
28.8 |
684 |
— |
— |
| Space Solar Panel |
CAVU Aerospace
|
149 |
960 |
— |
— |
— |
PDF
|
| SPEAR Probe |
Howe Industries
|
1540 |
3000 |
— |
— |
— |
— |
| Lunar Solar Power Plant |
Yuzhnoye Design Bureau
|
4110 |
10000 |
— |
— |
— |
— |
| 1U Battery Board |
CubeSat Aerospace
|
— |
— |
3.7 |
— |
— |
— |
| 1U Solar Panel |
Aphelion Orbitals
|
— |
150 |
|
— |
30.5% triple junction |
PDF
|
| 1U Solar Panels |
CubeSat Aerospace
|
— |
1 |
11.5 |
— |
— |
— |
| 24U CubeSat Solar Array (Very High Power) |
MMA Design
|
— |
330 |
— |
— |
— |
— |
| Advanced Solar Power Systems |
Astradyne
|
— |
10000 |
— |
— |
> 33% |
— |
| Airbus Space Battery Products |
Airbus Defence and Space
|
— |
— |
30 |
— |
— |
PDF
|
| BAT module |
Space Inventor ApS
|
— |
— |
14.4 |
— |
— |
— |
| Chiyu Solar Energy System |
Hongqing Technology (鸿擎科技)
|
— |
1000 |
— |
— |
— |
— |
| CLASP Composite Lightweight Array with Shape-memory Polymer |
CTD (Composite Technology Development)
|
— |
250 |
— |
— |
— |
PDF
|
| CubeSat Electrical Power System 1.0 (EPS) |
NanoAvionics
|
— |
175 |
— |
— |
— |
— |
| CubeSat GaAs Solar Panel |
NanoAvionics
|
— |
20 |
— |
— |
— |
— |
| CubeSat HDK Solar Array |
Ascent Solar Technologies
|
— |
2000 |
28 |
— |
— |
— |
| D-SP Deployable Solar Panels |
NPC Spacemind
|
— |
8.8 |
18.2–19.3 |
— |
— |
— |
| D-SP6X-L-1W |
NPC Spacemind
|
— |
18.4 |
18.4–20 |
— |
— |
— |
| DC/DC Converter |
Glavkosmos
|
— |
— |
2.8–5.5 |
— |
60–75% |
— |
| DROP-03 3U Deployable Solar panel |
2NDSpace Srl
|
— |
7.5 |
15.6 |
— |
— |
PDF
|
| DROP-08 8U/4U Deployable Solar panel |
2NDSpace Srl
|
— |
10 |
20.8 |
— |
— |
PDF
|
| DROP-12 12U Deployable Solar panel |
2NDSpace Srl
|
— |
20 |
20.8–41.6 |
— |
— |
PDF
|
| Electrical Power Systems (EPS) |
DHV Technology
|
— |
900 |
3.3–12 |
— |
— |
— |
| ELSA |
Deployable Space Systems (DSS) — now Redwire
|
— |
5000 |
— |
— |
— |
— |
| EP-500V HDK Solar Array |
Ascent Solar Technologies
|
— |
2000 |
500 |
— |
— |
— |
| External Power Supply |
Pumpkin, Inc.
|
— |
— |
5–6 |
— |
— |
— |
| Flexible Blanket Solar Array |
Dcubed
|
— |
2000 |
— |
— |
— |
— |
| Flexible High-Efficiency Space Solar Arrays |
Flexell
|
— |
— |
— |
— |
18–25% (thin-film multi-junction) |
— |
| GaInP/GaAs/Ge Lattice Matched 3J Solar Cells |
Spectrolab
|
— |
— |
— |
— |
up to 32% |
— |
| HaWK High Watts per Kilogram Solar Arrays |
MMA Design
|
— |
36 |
— |
— |
— |
— |
| High Voltage Power Supply System kit KPVS |
Glavkosmos
|
— |
60000 |
120 |
— |
— |
— |
| High-Power Electrical Power System Module (EPSM1) |
Pumpkin, Inc.
|
— |
300 |
16.8 |
— |
>99% |
PDF
|
| High-power Multi-channel Electrical Power System Module (EPSM1) |
Pumpkin, Inc.
|
— |
480 |
6–16.8 |
— |
>99% typical at moderate-to-high current |
— |
| Intelli-Pack |
Space Information Laboratories (SIL)
|
— |
45 |
— |
— |
— |
— |
| Intelligent Lithium Battery Module (BM2) |
Pumpkin, Inc.
|
— |
160 |
— |
100 |
— |
PDF
|
| Intelligent Protected Lithium Battery Module with SoC Reporting (BM2) |
Pumpkin, Inc.
|
— |
— |
5.2–16.8 |
— |
— |
PDF
|
| ISISPACE Compact Electrical Power System |
ISISPACE Group
|
— |
— |
3.3–5 |
— |
— |
PDF
|
| Large Deployable Solar Arrays |
Source Energy
|
— |
3000 |
— |
— |
— |
— |
| Latch-Up Current Limiter (LCL) |
3D Plus (HEICO)
|
— |
— |
0.8–5.5 |
— |
— |
— |
| Linear EPS Module (LEPSM1) |
Pumpkin, Inc.
|
— |
— |
6–8.4 |
— |
— |
PDF
|
| Modular Power Platform (MPP) |
Space Inventor ApS
|
— |
110 |
— |
— |
— |
— |
| NANOeps-AMPPT |
SkyLabs d.o.o.
|
— |
— |
12.1–23.3 |
— |
— |
— |
| Nanosatellite Battery Array |
Glavkosmos
|
— |
— |
14.8 |
— |
— |
— |
| Nanosatellite Electrical Power System |
Glavkosmos
|
— |
— |
3.3–5 |
— |
— |
— |
| Nanosatellite Power Subsystem |
Stellar Exploration, Inc.
|
— |
5000 |
— |
— |
— |
PDF
|
| Nanosatellite Solar Panel |
Glavkosmos
|
— |
2.1 |
— |
— |
— |
— |
| Optical Glass |
Glavkosmos
|
— |
— |
— |
80.5 |
— |
— |
| PCDU NANO Power Conditioning and Distribution Unit |
EREMS
|
— |
50 |
— |
— |
— |
— |
| Power Conditioning and Distribution Units (PCDU) |
Airbus Defence and Space
|
— |
23000 |
100 |
— |
— |
PDF
|
| Power Distribution Unit |
Space Inventor ApS
|
— |
— |
12 |
— |
— |
— |
| Power Supply (Various Models) |
Data Patterns (India) Ltd.
|
— |
5000 |
— |
— |
— |
— |
| PPS mk1 |
Kayser Space
|
— |
— |
28 |
— |
— |
— |
| PPS Power Distribution Units |
Kayser Space
|
— |
— |
28 |
— |
— |
— |
| PPU-1500 (Power Processing Unit) |
Space Electric Thruster Systems (SETS)
|
— |
1500 |
80–140 |
— |
Up to 94% |
PDF
|
| PPU-200 (Power Processing Unit) |
Space Electric Thruster Systems (SETS)
|
— |
80 |
26–36 |
— |
— |
PDF
|
| PPU-500 (Power Processing Unit) |
Space Electric Thruster Systems (SETS)
|
— |
500 |
24–36 |
— |
Up to 94% |
PDF
|
| PSR 100V MKII |
Airbus Defence and Space
|
— |
23000 |
100 |
— |
— |
PDF
|
| Ra Solar Panels |
Spacemanic s.r.o.
|
— |
— |
— |
— |
> 30% |
— |
| Rad-Hard DDR Termination Regulator |
3D Plus (HEICO)
|
— |
— |
1.6–2.8 |
— |
— |
— |
| ROSA Roll-Out Solar Array (Redwire / DSS) |
Deployable Space Systems (DSS) — now Redwire
|
— |
30000 |
12–300 |
— |
— |
— |
| ROSA — Roll-Out Solar Array |
Roccor (Redwire)
|
— |
— |
12–300 |
— |
— |
— |
| Rovial Breakthrough™ Solar Space Platform |
Rovial Space
|
— |
100000 |
— |
— |
— |
— |
| Satellite Solar Panels and Power Systems |
Azista Industries
|
— |
— |
— |
— |
~28–30% (triple-junction GaAs) |
— |
| SFC85N90S2 SiC Power MOSFET |
Solid State Devices Inc
|
— |
288 |
900 |
— |
— |
— |
| SFH06055-20 High Side Power Switch |
Solid State Devices Inc
|
— |
— |
60 |
— |
— |
— |
| SmallSat GaAs Deployable Solar Panels |
NanoAvionics
|
— |
0.037 |
— |
— |
— |
— |
| Smallsat HDK Solar Array |
Ascent Solar Technologies
|
— |
2000 |
28 |
— |
— |
— |
| Solar Arrays |
Blue Canyon Technologies
|
— |
27 |
14.9 |
— |
— |
PDF
|
| Solar Cell Battery |
Glavkosmos
|
— |
— |
4.5 |
— |
— |
— |
| Solar Element GaInP2 / GaAs / Ge |
Glavkosmos
|
— |
381 |
2371 |
80 |
— |
— |
| Solar Modules |
Source Energy
|
— |
303 |
— |
— |
— |
— |
| Solar Panel for AntS antenna |
Pumpkin, Inc.
|
— |
2 |
— |
— |
— |
— |
| Solar Panels for CubeSats |
DHV Technology
|
— |
2.4 |
— |
— |
— |
— |
| Solar Panels for Small Satellites |
DHV Technology
|
— |
100 |
— |
— |
— |
— |
| Space Point-of-Load (POL) DC/DC Converter |
3D Plus (HEICO)
|
— |
— |
5 |
— |
— |
— |
| Space Radiation Hardened Protection Switch |
3D Plus (HEICO)
|
— |
— |
3–12 |
— |
— |
— |
| Space-Grade DC-DC Converters |
EUROSATCOM
|
— |
2.5 |
12 |
— |
— |
— |
| SpaceTech SADA 44/22 (Solar Array Drive Assembly) |
SpaceTech GmbH
|
— |
— |
22–36 |
— |
— |
— |
| Supernova High Power PCDU |
Bradford Space
|
— |
300 |
28 |
— |
— |
— |
| SX-SBOX Power System (Microsatellite) |
SPUTNIX
|
— |
— |
22–34 |
— |
— |
— |
| SXC-PSS-03 Electrical Power System (with Battery Pack) |
SPUTNIX
|
— |
— |
6–8 |
— |
— |
— |
| Titan Bare Module |
Ascent Solar Technologies
|
— |
2100 |
20 |
— |
— |
— |
| VC91200 LUMIC Radiation-Hardened Latch-Up Monitor IC |
VORAGO Technologies
|
— |
— |
1.5–10 |
— |
— |
— |