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Mitsuru Imaizumi Space Solar Cells -- I -- HTV-6
Spacecraft Power System, Kyusyu Inst. Tech Oct. 19, 2018 Space Solar Cells -- I -- HTV-6 Mitsuru Imaizumi
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Contents Solar cell utilization in space Fundamentals of solar cells
Development history Radiation degradation Degradation prediction Recent R&D activities
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Contents Solar cell utilization in space Fundamentals of solar cells
Development history Radiation degradation Degradation prediction Recent R&D activities
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Solar Panels/Paddles GCOM-W1 GOSAT WINDS
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Solar Panels/Paddles HTV GMS-5 MMO 5
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Parallel number: Generation current Layout of solar cells in a panel
Solar Panels/Paddles Solar Paddle この表は、CSD搭載評価サンプルの名称と個数を示す。 7品種について2個ずつ搭載し、評価を実施している。 打上後の初期チェックアウト時に、各評価デバイスについて電気特性のデータを取得し、 全て正常に機能し、データが得られていることを確認した。 Series number: Generation voltage Output voltage Output current Parallel number: Generation current Layout of solar cells in a panel 6
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High efficiency Si solar cell InGaP/GaAs/Ge triple-junction solar cell
Space Solar Cells Buried bypass diodes Bypass diode Interconnector Cell size: 2×2 cm2 Size: 40mm×60mm Size: 37mm×76mm High efficiency Si solar cell InGaP/GaAs/Ge triple-junction solar cell
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A coupon solar panel with Si solar cells for testing
Space Solar Panel Cell size: 2×2 cm2 A coupon solar panel with Si solar cells for testing
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Structure of Solar Panels
Solar cell Coverglass Adhesive Electrodes AR coating Polyimide film Aluminum Honeycomb CFRP Cross-sectional schematic of a solar panel (not to scale)
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Contents Solar cell utilization in space Fundamentals of solar cells
Development history Radiation degradation Degradation prediction Recent R&D activities
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Current-Voltage Characteristics
Current-voltage (I-V) characteristics of a solar cell
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A typical current-voltage (I-V) curve
Output Parameters A typical current-voltage (I-V) curve
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Equivalent Circuit of Solar Cells
Id Vd Rs = 0 Iph Rsh = ∞ V n = 1 Ish Equivalent circuit of a (single-junction) solar cell
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Contents Solar cell utilization in space Fundamentals of solar cells
Development history Radiation degradation Degradation prediction Recent R&D activities
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High efficiency Si solar cell InGaP/GaAs/Ge triple-junction solar cell
Space Solar Cells Buried bypass diodes Bypass diode Inter-connector Cell size: 2×2 cm2 Size: 40mm×60mm Size: 37mm×76mm High efficiency Si solar cell InGaP/GaAs/Ge triple-junction solar cell
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Structure of Si Space Solar Cell
Schematic cross-sectional structure of the “HES” Si space solar cell
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Back-Surface Field Layer
n-type Emitter Depletion Layer p-type Base n-type Emitter Depletion Layer p-type Base BSF no BSF layer with BSF layer Effect of insertion of the back-surface field (BSF) layer
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Back-Surface Reflection Layer
Solar Cell Substrate Visible light Infrared (unabsorbed) light Substrate BSR Solar Cell Visible light Infrared (unabsorbed) light no BSR layer with BSR layer Effect of insertion of the back-surface reflection (BSR) layer
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Non-Reflection Surface Structure
Solar Cell Reflection ARC Texture Solar Cell ARC Reflection Flat surface Textured surface Effect of the textured non-reflection surface (NRS) structure
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Efficiency of Space Solar Cells
Historical improvement of the efficiency of space solar cells
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High efficiency Si solar cell InGaP/GaAs/Ge triple-junction solar cell
Space Solar Cells Buried bypass diodes Bypass diode Inter-connector Cell size: 2×2 cm2 Size: 40mm×60mm Size: 37mm×76mm High efficiency Si solar cell InGaP/GaAs/Ge triple-junction solar cell
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Structure of 3J Space Solar Cell
Cross-sectional structure of an InGaP/GaAs/Ge triple-junction (3J) solar cell
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Current-Voltage Charateristics of 3J Cell
A typical current-voltage (I-V) characteristics of an InGaP/GaAs/Ge 3J solar cell
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Efficiency of Space Solar Cells
Historical improvement of the efficiency of space solar cells
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Effect of Efficiency Improvement
HES solar cell (η=17%) 3J solar cell (η=27%) Area reduction of about 60% この表は、CSD搭載評価サンプルの名称と個数を示す。 7品種について2個ずつ搭載し、評価を実施している。 打上後の初期チェックアウト時に、各評価デバイスについて電気特性のデータを取得し、 全て正常に機能し、データが得られていることを確認した。 Effect of improvement of solar cell efficiency (paddle-size reduction)
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Contents Solar cell utilization in space Fundamentals of solar cells
Development history Radiation degradation Degradation prediction Recent R&D activities
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Space Environment for Solar Cells
Radiation (High energy electrons/protons) High/low temperature and thermal cycles Ultraviolet Charging/discharging Mechanical vibration and sonic wave Debris/meteoroids (particle)
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Requirements for Space Solar Cells
Efficiency … but not at BOL but at EOL Radiation resistance Lightweight Thermal (cycle) durability Mechanical strength Inexpensiveness
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Structure of Solar Panel Cross-sectional schematic of a solar panel
Solar cell Coverglass Adhesive Electrodes AR coating Polyimide film Aluminum Honeycomb CFRP Cross-sectional schematic of a solar panel
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Radiation Degradation of Output
High fluence Cell size: 2×2 cm2 Degradation on I-V characteristics Beginning-of-life (BOL) and end-of-life (EOL) Degradation of solar cell output due to radiation exposure
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Decrease in Output Parameters
Absolute values Remaining factors Degradation trend of HES solar cell due to 10 MeV proton irradiation
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Contents Solar cell utilization in space Fundamentals of solar cells
Development history Radiation degradation Degradation prediction Recent R&D activities
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Prediction of Radiation Degradation
Difference between ground tests and actual space to be considered Ground tests Actual space Normal incidence Mono energy No shielding Omni-directional incidence (4π) Multi energy Shielding effects Front: coverglass Back: substrate
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Radiation Environment
An example of the chronal change in dose rates of protons and electrons
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Radiation Environment
An example of the dependency of proton dose rates on proton energy
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An example of the dependency of degradation curves on proton energy
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Relative Damage Coefficients
Reference energy Electrons: 1 MeV Protons: 10MeV An example of the relative damage coefficients for protons
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Prediction of Radiation Degradation
Matters to be considered and estimated Reduction of energy and dose rate due to shielding effect by coverglass etc. Effective penetration depth depending on incident angle.
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Equivalent Fluence Calculation of the equivalent 1 MeV electron fluence 1 MeV electron / 10 MeV proton conversion factor: k Isc Voc Pmax 4350 1280 2580 For HES cell
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Prediction of Radiation Degradation
An example of estimation of degradation rate from the equivalent 1 MeV electron fluence
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Contents Solar cell utilization in space Fundamentals of solar cells
Development history Radiation degradation Degradation prediction Recent R&D activities
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Recent R&D Activity on Space Solar Cells
Realize a high specific power solar paddle Require 1. A high specific power solar cell in a sheet (1.0W/g) An ultra-lightweight panel structure
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Recent R&D Activity on Space Solar Cells
InGaAs bottom-cell InGaAs bottom-cell InGaP top-cell GaAs bottom-cell Ge substarte InGaP top-cell GaAs middle-cell InGaAs bottom-cell Drastic weight reduction and flexibilization of multi-junction high-efficiency space solar cells by removal of “heavy” Ge substrate
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Recent R&D Activity on Space Solar Cells
Current 3J cell (150μm thick, 2.2 grams) Developed 3J cell (30μm thick, 0.25 grams)
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Recent R&D Activity on Space Solar Panels
Supporting layer Thin 3J cell Front contact Back contact Thin-film cell Laminating Film Adhesive Interconnector N-side tab P-side tab Cell-array sheet Lightweight panel Solar cell sheet Panel frame
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Recent R&D Activity on Space Solar Cells
27.4 cm2, 330 mg, ~30μm AM0, InGaP/GaAs/InGaAs Triple-junction Solar Cell Specific Power: 3.6 W/g
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Recent R&D Activity on Space Solar Sheets Cross section structure
Thin coverglass Adhesive IMM-3J Cell Backsheet material Cross section structure Thickness: ~ 0.3 mm Weight: ~30 g Specific Power: 0.58 W/g
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Recent R&D Activity on Space Solar Panels
Demonstration panel has been mounted on a vacant panel slot on HTV-6 Space Demonstration Test
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Recent R&D Activity on Space Solar Panels Lightweight Solar Paddle
Stowed Deployed Lightweight Solar Paddle
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Recent R&D Activity on Space Solar Panels
Features: Lightweight, Compact, but Tough Curved, thin frame Lightweight and thin frame + SSS SSSs applied with Velcro fasteners
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Recent R&D Activity on Space Solar Panels
Innovative Technology Demonstration Sat-1
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