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48 lines
1.8 KiB
Python
48 lines
1.8 KiB
Python
# ==============================================================================
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# COPYRIGHT NO ONE EVERYWHERE LLC (WYOMING HOLDING COMPANY)
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# PROJECT: SOVEREIGN STACK
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# This artifact is entirely proprietary and cryptographically proven.
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# Open-Source usage requires explicit permission from Brandon Scott Schneider.
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# ==============================================================================
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from math_harness_compat import xp, AnyArray
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# Let's map the engine capabilities across multiple planetary atmospheres
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def map_planetary_thermodynamics():
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# Base target values
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delta_t = 45.0 # Degrees C
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flow_rate = 0.5 # m^3/sec
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planets = {
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"Earth (Sea Level)": {
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"density": 1.225, # kg/m^3
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"cp": 1005 # J/(kg*K)
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},
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"Mars (Surface)": {
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"density": 0.020, # kg/m^3 (Mostly CO2)
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"cp": 760 # J/(kg*K) for CO2 at ~-60°C, 6 mbar (Mars surface)
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},
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"Venus (Surface)": {
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"density": 65.0, # kg/m^3 (Massive CO2 pressure)
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"cp": 1100 # J/(kg*K) super-critical CO2
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},
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"Titan (Surface)": {
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"density": 5.42, # kg/m^3 (Cold dense N2/CH4)
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"cp": 1040 # J/(kg*K) for Nitrogen
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},
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"Jupiter (High Alt - 1 Bar)": {
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"density": 0.16, # kg/m^3 (H2/He gas)
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"cp": 12640 # J/(kg*K) mass-weighted H2/He mix (90%/10%)
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}
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}
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print("Planetary Thermal Extraction Profile (0.5 m^3/s Flow @ 45C Delta T)")
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print("-" * 75)
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print(f"{'Environment':<25} | {'Mass Flow (kg/s)':<18} | {'Power Yield (kW)':<15}")
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print("-" * 75)
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for planet, data in planets.items():
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mass_flow = data["density"] * flow_rate
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power_w = mass_flow * data["cp"] * delta_t
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print(f"{planet:<25} | {mass_flow:<18.3f} | {power_w/1000.0:<15.2f}")
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map_planetary_thermodynamics()
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