# ==============================================================================
# COPYRIGHT NO ONE EVERYWHERE LLC (WYOMING HOLDING COMPANY)
# PROJECT: SOVEREIGN STACK
# This artifact is entirely proprietary and cryptographically proven.
# Open-Source usage requires explicit permission from Brandon Scott Schneider.
# ==============================================================================
from math_harness_compat import xp, AnyArray

# Let's map the engine capabilities across multiple planetary atmospheres
def map_planetary_thermodynamics():
    # Base target values
    delta_t = 45.0 # Degrees C
    flow_rate = 0.5 # m^3/sec

    planets = {
        "Earth (Sea Level)": {
            "density": 1.225, # kg/m^3
            "cp": 1005 # J/(kg*K)
        },
        "Mars (Surface)": {
            "density": 0.020, # kg/m^3 (Mostly CO2)
            "cp": 760 # J/(kg*K) for CO2 at ~-60°C, 6 mbar (Mars surface)
        },
        "Venus (Surface)": {
            "density": 65.0, # kg/m^3 (Massive CO2 pressure)
            "cp": 1100 # J/(kg*K) super-critical CO2
        },
        "Titan (Surface)": {
            "density": 5.42, # kg/m^3 (Cold dense N2/CH4)
            "cp": 1040 # J/(kg*K) for Nitrogen
        },
        "Jupiter (High Alt - 1 Bar)": {
            "density": 0.16, # kg/m^3 (H2/He gas)
            "cp": 12640 # J/(kg*K) mass-weighted H2/He mix (90%/10%)
        }
    }
    
    print("Planetary Thermal Extraction Profile (0.5 m^3/s Flow @ 45C Delta T)")
    print("-" * 75)
    print(f"{'Environment':<25} | {'Mass Flow (kg/s)':<18} | {'Power Yield (kW)':<15}")
    print("-" * 75)
    
    for planet, data in planets.items():
        mass_flow = data["density"] * flow_rate
        power_w = mass_flow * data["cp"] * delta_t
        print(f"{planet:<25} | {mass_flow:<18.3f} | {power_w/1000.0:<15.2f}")

map_planetary_thermodynamics()