Achieving solar tracking and attitude determination for small satellites with high-sensitivity sensors.
The nanoSSOC-A60 is a sun sensor utilizing solar tracking technology. This product is designed to provide high precision in solar tracking, orientation, and attitude determination specifically for nano-satellite platforms like Cubesats. The nanoSSOC-A60 features advanced engineering by creating a highly integrated sensing structure. Its small size, lightweight, and low power consumption offer an ideal ADCS solution that ensures efficient and reliable performance in space. Key features include: - A dual-axis sun sensor for accurate tracking and determination. - High sensitivity based on geometric design dimensions. - Utilization of MEMS technology for high integration. - Optimal for nano-satellite platforms due to its small size and low power consumption. - Use of space-grade electronic components. - Compatibility with most cubesat structures and OBCs. - Robust against extreme temperatures and radiation. With over 50 units used in more than 10 missions, the reliability and efficiency of the nanoSSOC-A60 are well proven, making it ideal for space missions that require accurate and reliable solar tracking capabilities.
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basic information
nanoSSOC-A60 Sun Sensor: Detailed Overview - Type: 2-axis orthogonal sun sensor - Field of View: ±60º - Accuracy: <0.5º (3 sigma), <0.1º (precision) - Electrical Interface: 4 voltage outputs, 10-pin micro connector - Power Supply: 3.3V / 5V, <2mA consumption - Mechanical Interface: 27.4 x 14 x 5.9 mm, weight 4g - Housing: Aluminum 6082 with black anodized finish - Operating Temperature: -30℃ to 85℃ - Radiation Resistance: >100 kRad (gamma), 6 MeV 3000 kRad (proton) - Vibration and Shock Resistance: Random vibration 14.1g @ 20 -2000 Hz, shock 3000 g @ 1 -100 ms This comprehensive specification set highlights the capabilities and design of the nanoSSOC-A60, emphasizing its suitability for challenging space missions.
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The nanoSSOC-A60 sun sensor is a versatile tool that enhances the capabilities of nano-satellite missions across various applications: - Improves the accuracy of solar tracking, optimizes the positioning of solar panels, and maximizes energy intake. - Provides precise attitude determination to ensure optimal orientation for scientific instruments and communication antennas. - Enhances the performance of ADCS (Attitude Determination and Control System) in cubesats, promoting better mission outcomes. - Ensures reliable operation in extreme space conditions through robust design and space-grade components. - Integrates with most cubesat structures and onboard computers (OBC) to provide flexible solutions for various mission designs. These applications emphasize the role of the nanoSSOC-A60 in advancing nano-satellite technology by providing reliable and efficient solutions for space exploration and research.
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Company information
Rikei Corporation was established in 1957 and is a solution vendor in the IT and electronics industry, celebrating its 65th anniversary. We propose a variety of solutions centered around cutting-edge technologies and advanced products in the fields of system solutions, network solutions, and electronic components and devices, tailored as the optimal "step-ahead solution" to meet our customers' needs.
