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Engineered for nanosatellites, this sun sensor offers great performance in a compact and lightweight design with low power usage.","dualUse":true,"faqs":[{"_key":"faq-0","_type":"productFaq","answer":["For Eagle, use the published < ±0.15° accuracy, 3σ value in the ADCS error budget. Precision should not be used as a substitute for system-level accuracy."],"question":"What accuracy value should be used in the ADCS error budget?"},{"_key":"faq-1","_type":"productFaq","answer":["Accuracy describes how close the measured sun angle is to the true sun angle. Precision describes repeatability or measurement noise. For ADCS budgeting, use the accuracy value; for filtering and noise assumptions, use the precision value."],"question":"What is the difference between the published accuracy and precision values?"},{"_key":"faq-2","_type":"productFaq","answer":["Yes. Each delivered Eagle sun sensor is individually characterized and delivered with a calibration matrix linked to its specific serial number. The correct matrix should be used with the matching flight unit."],"question":"Is the calibration matrix linked to each delivered serial number?"},{"_key":"faq-3","_type":"productFaq","answer":["The calibration step defines how densely the sensor is characterized across its angular measurement range. Eagle is calibrated by default with a 10° angular step, while optional paid 5° and 2° calibration provide a denser calibration dataset.","A smaller step means more calibration points, which can be useful for missions that require higher confidence in the sensor model or stricter ADCS validation. The calibration step should be selected before order confirmation because it affects calibration effort, price, and potentially lead time."],"question":"What is the difference between 10°, 5°, and 2° sun sensor calibration?"},{"_key":"faq-4","_type":"productFaq","answer":["Eagle outputs measured sun-angle data for ADCS integration. To achieve the published angular accuracy, the customer should apply the serial-number-linked calibration matrix on the ADCS side.","The calibration matrix compensates sensor linearity and is delivered for the specific sensor serial number."],"question":"Does Eagle output calibrated angles?"},{"_key":"faq-5","_type":"productFaq","answer":["Eagle uses an I2C interface, making it suitable for compact CubeSat architectures where the sun sensor is close to the onboard computer and internal harness lengths are short.","I2C is commonly appropriate for 1–3U CubeSats with simple local bus integration. For larger CubeSats, SmallSats, longer harnesses, or missions requiring a more robust differential interface, Eagle Plus with RS485 may provide more integration margin."],"question":"Is I2C suitable for our mission?"},{"_key":"faq-6","_type":"productFaq","answer":["Eagle provides a 10 Hz measurement update rate, suitable for typical CubeSat ADCS polling and sun-vector acquisition use cases."],"question":"What is the expected measurement update rate?"},{"_key":"faq-7","_type":"productFaq","answer":["Mount Eagle on a stable, flat, and well-defined spacecraft surface according to the mechanical ICD. Avoid deformation, shadowing, reflections, contamination, and uncontrolled mounting tolerances, as these can reduce spacecraft-level angular accuracy."],"question":"How should Eagle be mounted to preserve angular accuracy?"},{"_key":"faq-8","_type":"productFaq","answer":["Spacecraft-level alignment tolerance should be budgeted separately from the sensor accuracy. ADCS teams should include mounting tolerance, panel flatness, thermoelastic deformation, and reference-frame transformation errors in the total pointing knowledge budget."],"question":"What alignment tolerance should be considered at spacecraft level?"},{"_key":"faq-9","_type":"productFaq","answer":["A typical full-sky CubeSat configuration uses six sun sensors mounted on the ±X, ±Y, and ±Z faces. Fewer sensors may be sufficient if the mission has limited attitude modes or does not require full-sky sun visibility."],"question":"How many sun sensors are typically needed for full-sky coverage?"},{"_key":"faq-10","_type":"productFaq","answer":["For early software and communication testing, Needronix provides Eagle sun sensor simulators as a lower-cost alternative to engineering models. The simulator reproduces the sensor bus communication and health-data exchange, but does not include the optical detector.","It can be used in a standard office or FlatSat environment, allowing software teams to test communication, debug integration issues, and prepare ADCS software before working with flight hardware. Simulators are available at €300 per unit."],"question":"Do you provide engineering models or simulators?"},{"_key":"faq-11","_type":"productFaq","answer":["Each Eagle unit is delivered with a serial-number-linked calibration matrix. Along with ICDs and user manuals, Needronix also provides ready-to-use Python scripts to support first connection, bench testing, FlatSat validation, debugging, and ADCS software integration."],"question":"What is included to support Eagle integration?"},{"_key":"faq-12","_type":"productFaq","answer":["Yes. Eagle can be procured repeatedly in the same configuration for CubeSat programmes. Interface configuration, mechanical configuration, calibration option, documentation package, and acceptance requirements should be frozen early to maintain repeatability across multiple flight units."],"question":"Can the same Eagle configuration be procured repeatedly for a CubeSat programme?"},{"_key":"faq-13","_type":"productFaq","answer":["Export-control review may be required depending on destination country, end user, delivery country, and mission application. 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For compact 1–3U spacecraft with very short harnesses, Eagle with I2C may also be sufficient, while Eagle Plus with RS485 provides more integration margin for demanding missions."],"question":"Is RS485 suitable for our mission?"},{"_key":"faq-6","_type":"productFaq","answer":["Mount Eagle Plus on a stable, flat, and well-defined spacecraft surface according to the mechanical ICD. Avoid deformation, shadowing, reflections, contamination, and uncontrolled mounting tolerances, as these can reduce spacecraft-level angular accuracy."],"question":"How should Eagle Plus be mounted to preserve angular accuracy?"},{"_key":"faq-7","_type":"productFaq","answer":["Spacecraft-level alignment tolerance should be budgeted separately from the sensor accuracy. 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