{ 'description': '\n' ' Demonstration of the PADRE spacecraft assessment mode. ' 'This analysis simulated the \n' ' destructive re-entry of a 1000kg component-centric ' 'vehicle, modelled as a relatively \n' ' simple structore comprising approximately 40 components. ' 'Re-entry is predicted from \n' ' a circular sun-synchronous orbit of 130km altitude using ' 'SAMj. Uncertainties in the \n' ' initial state vector, atmosphere density, material ' 'properties, drag and heating \n' ' coefficients are considered. A standard Monte-Carlo of ' 'between 1000 simulations has \n' ' been executed.\n' ' ', 'draSra': True, 'initialState': { 'argumentPerigee': 0, 'attack': 0, 'bank': 0, 'eccentricity': 0, 'emissivityAlLi': 0.16, 'emissivityAluminium': 0.4, 'emissivityAluminiumOxide': 0.8, 'emissivityBatteryLithium': 0.5, 'emissivityBatteryNiCd': 0.5, 'emissivityBeryllium': 0.8, 'emissivityBorosilicate': 0.8, 'emissivityBrass': 0.22, 'emissivityCarbonCarbon': 0.85, 'emissivityCfrp': 0.8, 'emissivityCfrpL20': 0.9, 'emissivityCfrpLy556': 0.9, 'emissivityCfrpPeak': 0.9, 'emissivityChromite': 0.9, 'emissivityCobalt': 0.75, 'emissivityCopper': 0.6, 'emissivityCsI': 0.8, 'emissivityElectronics': 0.4, 'emissivityFusedSilica': 0.8, 'emissivityGermanium': 0.1, 'emissivityGfrp': 0.9, 'emissivityGfrpSbi': 0.8, 'emissivityGfrpTufnol': 0.65, 'emissivityHaynes25': 0.95, 'emissivityHaynes25Oxide': 0.95, 'emissivityHc4Ply': 0.8, 'emissivityHc8Ply': 0.8, 'emissivityHiperco': 0.75, 'emissivityInconel': 0.9, 'emissivityInermet': 0.1544, 'emissivityInvar': 0.7, 'emissivityIron': 0.85, 'emissivityLanthanum': 0.41, 'emissivityLead': 0.8, 'emissivityMagnefier': 0.75, 'emissivityMagnefierMelt': 0.5, 'emissivityMolybdenum': 0.8, 'emissivityNextel': 0.8, 'emissivityNickelIron': 0.8, 'emissivityPlatinumRhodium': 0.8, 'emissivityPotting': 0.8, 'emissivitySanidine': 0.93, 'emissivitySiC': 0.85, 'emissivitySilicone': 0.8, 'emissivitySolarPanel': 0.4, 'emissivitySteel': 0.85, 'emissivitySteelcan': 0.87, 'emissivityTantalum': 0.8, 'emissivityTitanium': 0.77, 'emissivityTungsten': 0.5, 'emissivityZerodur': 0.8, 'emissivityZnSe': 0.8, 'energyThreshold': 15, 'epoch': '2026-12-01 02:07:25', 'heatFluxContFree': 0.3333, 'latHeatAlLi': 361500.0, 'latHeatAluminium': 400000.0, 'latHeatAluminiumOxide': 1093000.0, 'latHeatBatteryLithium': 261000.0, 'latHeatBatteryNiCd': 174500.0, 'latHeatBeryllium': 1133000, 'latHeatBrass': 168000.0, 'latHeatCarbonCarbon': 365000, 'latHeatCfrpPeak': 4500000, 'latHeatChromite': 91600, 'latHeatCobalt': 275000, 'latHeatCopper': 243000, 'latHeatCsI': 1, 'latHeatElectronics': 49000, 'latHeatFusedSilica': 10000000, 'latHeatGermanium': 466500, 'latHeatGfrp': 800232.6, 'latHeatGfrpTufnol': 800232.6, 'latHeatHaynes25': 275000, 'latHeatHaynes25Oxide': 1500000, 'latHeatHc4Ply': 400000.0, 'latHeatHc8Ply': 400000.0, 'latHeatHiperco': 275000, 'latHeatInconel': 309000, 'latHeatInermet': 189800.0, 'latHeatInvar': 274000, 'latHeatIron': 272000, 'latHeatLanthanum': 44600, 'latHeatLead': 1, 'latHeatMagnefier': 270000, 'latHeatMolybdenum': 374800, 'latHeatNextel': 1093000, 'latHeatNickelIron': 271300, 'latHeatPlatinumRhodium': 120000, 'latHeatPotting': 3000000, 'latHeatSanidine': 226400, 'latHeatSiC': 365000, 'latHeatSilicone': 1000000, 'latHeatSolarPanel': 361459.0, 'latHeatSteel': 270300, 'latHeatSteelcan': 278000, 'latHeatTantalum': 1, 'latHeatTitanium': 337700, 'latHeatTungsten': 192000.0, 'latHeatZerodur': 4000000, 'latHeatZnSe': 10, 'meltTempAlLi': 906.15, 'meltTempAluminium': 850.0, 'meltTempAluminiumOxide': 2327.0, 'meltTempBatteryLithium': 630.0, 'meltTempBatteryNiCd': 1160.0, 'meltTempBeryllium': 1550, 'meltTempBrass': 1318.0, 'meltTempCarbonCarbon': 3600, 'meltTempCfrp': 1000, 'meltTempCfrpPeak': 525, 'meltTempChromite': 2123, 'meltTempCobalt': 1753, 'meltTempCopper': 1356, 'meltTempCsI': 905, 'meltTempElectronics': 646, 'meltTempFusedSilica': 2600, 'meltTempGermanium': 1211, 'meltTempGfrp': 1473, 'meltTempGfrpTufnol': 1473, 'meltTempHaynes25': 1643, 'meltTempHaynes25Oxide': 1800, 'meltTempHc4Ply': 890.0, 'meltTempHc8Ply': 930.0, 'meltTempHiperco': 1753.0, 'meltTempInconel': 1630, 'meltTempInermet': 2708.0, 'meltTempInvar': 1700, 'meltTempIron': 1808, 'meltTempLanthanum': 1188, 'meltTempLead': 600, 'meltTempMagnefier': 1718, 'meltTempMolybdenum': 2896, 'meltTempNextel': 1700, 'meltTempNickelIron': 1703, 'meltTempPlatinumRhodium': 2123, 'meltTempPotting': 1900, 'meltTempSanidine': 1963, 'meltTempSiC': 3100, 'meltTempSilicone': 800, 'meltTempSolarPanel': 906.15, 'meltTempSteel': 1665.0, 'meltTempSteelcan': 1658.0, 'meltTempTantalum': 3258, 'meltTempTitanium': 1905, 'meltTempTungsten': 3695.0, 'meltTempZerodur': 1558, 'meltTempZnSe': 920, 'pitchRate': 0, 'raan': -45, 'rollRate': 0, 'semiMajorAxis': 6501000, 'sideslip': 0, 'simMode': 3, 'type': 'kepler', 'voxelMode': 1, 'voxelSize': 0.005, 'yawRate': 0}, 'maxSimulationCount': 1000, 'minSimulationCount': 1000, 'outputDirectory': 'Output3', 'propagator': {'threadCount': 3, 'type': 'samj'}, 'reentryType': 'controlled', 'risk': { 'growthScenario': 'MEDIUM-VARIANT', 'threadCount': 3, 'type': 'seram'}, 'statistics': {'algorithm': 'monteCarlo', 'batchSize': 250}, 'template': 'Spacecraft', 'title': 'Example SAMj Controlled Component-Centric Vehicle Re-entry'}