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Dimensions: 16.6m length, 1.8m diameter
Mission: Geological exploration of Proxima b and atmospheric analysis
Features: Modular design, high-resolution optical and thermal imaging arrays, and multi-spectrum sensors
Technology: DCMCAAFR compact reactor, magnetic nozzle, advanced fuel systems, AURAI autonomous control
The Alpha Centauri Exploratory Probe (ACEP) is a highly sophisticated autonomous spacecraft meticulously engineered to perform comprehensive scientific investigations of Proxima b, an exoplanet of significant astrobiological interest in the Alpha Centauri star system. Its primary objectives encompass the characterization of Proxima b's geological features, atmospheric composition, and environmental parameters, ultimately generating critical datasets to support future interstellar exploration initiatives.
ACEP's propulsion architecture is driven by the compact Dual-Core Magnetically Confined Antimatter Augmented Fusion Reactor (DCMCAAFR), providing sustained high-energy output and advanced thrust capabilities. An integrated magnetic nozzle assembly enables precise modulation of plasma exhaust for optimal propulsion efficiency. The spacecraft's autonomous operations are orchestrated by the AURAI system, which dynamically regulates propulsion, energy distribution, and data acquisition protocols in real time, thereby minimizing dependence on Earth-based oversight and compensating for significant interstellar communication latencies.
The probe's instrumentation suite includes high-resolution optical cameras and thermal imaging devices for granular surface mapping, as well as atmospheric composition sensors employing mass spectrometry and gas chromatography to detect and analyze key gaseous constituents. LIDAR systems generate high-precision topographical data, refining the understanding of Proxima b's surface morphology. Complementing these capabilities is the ACEP Atmos probe, a specialized descent vehicle designed to penetrate the planet's atmosphere and collect in situ measurements of pressure, temperature, and gas composition. Its findings are relayed to the primary spacecraft during a predetermined operational window, providing invaluable insight before completing its terminal descent.
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Speed 0 equals LEO velocity at 200 km altitude