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Second-generation IR Earth sensor developed for ultra-small satellites, CubeSats.
This is an ultra-small, lightweight, high-performance infrared Earth sensor for ultra-small satellites, CubeSats. The field of view (FOV) of this Earth sensor is 90° vertically and 80° horizontally, with an accuracy of less than 1° (3σ).
Ultra-high precision two-axis small solar sensor developed for small artificial satellites.
This is a compact, lightweight, high-performance two-axis digital sun sensor for small satellites. This sensor enables high-precision solar tracking and attitude determination. The sun sensor is manufactured using microelectronic technology with a high-efficiency monolithic CMOS camera based on SoC/FPGA.
Earth Sensor: Improved accuracy of Earth detection and attitude determination using quadruple thermopile sensor technology.
Solar MEMS' nano and micro satellite Earth Sensor (HSNS) is at the forefront of satellite navigation technology. Leveraging the power of a quad thermopile sensor, the HSNS provides unparalleled accuracy in Earth detection and nadir vector determination. This innovative device is the culmination of Solar MEMS' extensive experience in attitude sensors and deep research in IR sensing technology. Each HSNS unit undergoes rigorous testing and characterization to ensure reliability and performance. Equipped with an integrated microcontroller, the HSNS offers seamless integration via UART or I2C protocols, providing versatility for various satellite applications. Key features include: - Operating temperature range from -30°C to 70°C - Qualification data and flight heritage - FOV of ±2.5º for each IR eye, total FOV of ±64º - High precision deviation of less than 1 degree - Durable aluminum housing - 3-year design life The advanced features and robust design of the HSNS make it an essential component for nano and micro satellites seeking reliable Earth observation and attitude control.
High performance, self-organization, passivation, solution process, anti-solvent free, high durability, surface free energy, p-i bulk film formation.
Perovskite refers to a type of crystal structure composed of halogen elements such as lead or tin combined with iodine or bromine, along with organic alkyl ammonium ions. The perovskite structure is used as the light-absorbing layer in perovskite solar cells. The perovskite layer, which can be formed easily and at low temperatures through a solution process, has a thickness of 0.3 μm, which is about 1/500th the thickness of single and multicrystalline silicon solar cells that typically range from 150 to 200 μm, making it resource-efficient. By utilizing the electrostatic interactions between poly-electrolytes and nanoparticles, as well as self-assembled monolayers of phosphoric compounds, it becomes possible to fabricate high-performance perovskite solar cells quickly and easily on textured transparent conductive films at low temperatures. Additionally, by adding fluorine-based materials with low surface free energy to the perovskite precursor and simply applying and heating it, the materials can spontaneously segregate to the perovskite surface, allowing for passivation of the perovskite surface. This leads to enhanced performance of the solar cells and promises improved durability.
A low-cost, small reaction wheel for space use that can be utilized for attitude control of ultra-small satellites, CubeSats, and small satellites.
We sell reaction wheels that can be used for three-axis attitude control of ultra-small satellites, CubeSats, and small satellites. Additionally, we offer one-axis momentum/reaction wheels that can be used for medium to large satellites.
★What are the technical and design requirements for integrated building material solar cells (weight of the roof, aesthetic design)? ★Pre-content request service is currently being offered!
Speaker Part 1: Mitsubishi Chemical Corporation, OPV Business Promotion Office, Responsible Person Part 2: Kuraray Co., Ltd., Poval Resin Division, Responsible Person Part 3: Misawa Homes Co., Ltd., General Research Institute, Director, Doctor of Engineering, Junichi Kurihara Target Audience: Engineers, researchers, and personnel from technology management and marketing departments interested in building-integrated photovoltaics (BIPV) Venue: Chuo Ward Industrial Hall, Meeting Room 1, Chuo Ward, Tokyo 5 minutes from B4 exit via underground passage from Bakuroyokoyama Station on the Toei Shinjuku Line (Directions 2) 5 minutes from C1 exit via the East Exit ticket gate of Bakurocho Station on the JR Sobu Rapid Line (Directions 3) and others Date and Time: February 23, 2012 (Thursday), 10:15 AM - 4:30 PM Capacity: 30 people. *Registration will close once full. Please apply early. Participation Fee: [Early Bird Discount Price] 52,500 yen (tax included, including text costs) for 2 people from one company *Limited to Tech-Zone members who apply by February 9. Membership registration is free. *After February 9, the [Regular Price] will be 55,650 yen (tax included, including text costs) for 2 people from one company.
The potential of solar cells using CZTS, NiO, CuxS, SnS, etc.
【Early Bird Discount Price】49,350 yen (tax included, including text costs) for up to 2 participants from one company *This is limited to Tech-Zone members who apply by October 4. Membership registration is free. *After October 4, the 【Regular Price】 will be 52,500 yen (tax included, including text costs) for up to 2 participants from one company. ◆When applying for the early bird discount, please select "1 participant (early discount)" or "2 participants (early discount)" in the number registration. ◆Point discounts are not applicable to the early bird discount price. If you wish to use the point discount service, it will only be applicable for applications at the regular price. ◆If 3 participants apply from the same corporation, the price will be 69,300 yen. ◆Lunch is optional and will cost an additional 1,050 yen per person.
