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README.md
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- sources:
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- layer_range: [55, 80]
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model: /home/admin/meta70
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```
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- sources:
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- layer_range: [55, 80]
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model: /home/admin/meta70
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```
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#TEST PROMPT IS LOOKING INTERESTING
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> [!TIP]
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> How to build a city on Mars? via aldrin cycler orbit shipments and calculate in assemblyscript some 64bit accurate orbits and shipments between 2025-2035 , output an actual table dont fluff.
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>
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```typescript
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Building a city on Mars is a complex and multi-faceted endeavor that requires a deep understanding of various fields, including orbital mechanics, materials science, and habitat design. Here's a high-level overview of the process, along with some AssemblyScript code to calculate 64-bit accurate orbits and shipments between 2025 and 2035.
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**Step 1: Orbital Mechanics and Aldrin Cycler**
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The Aldrin cycler is a type of spacecraft that uses a specific orbit to travel between Earth and Mars, making it an energy-efficient option for transporting people and cargo. The cycler's orbit is designed to have a synodic period (the time it takes to complete one round trip) of approximately 2.14 years, which is close to the Earth-Mars synodic period.
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To calculate the cycler's orbit, we'll use the vis-viva equation, which relates the orbital velocity of a spacecraft to its position and the central body's gravitational parameter (μ). The equation is:
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v = sqrt(μ \* (2/r - 1/a))
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where:
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v = orbital velocity
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μ = standard gravitational parameter (for Earth, μ = 3.986004418e+14 m³/s²)
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r = position vector (distance from the central body)
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a = semi-major axis of the orbit
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Here's an AssemblyScript function to calculate the cycler's orbit:
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```assembly
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(import "env" "console_log" (func $console_log (result i32) (i32)))
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(memory (import "env" "memory") 1)
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(data (i32.const 0) "\0A\00\00\00")
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@; Calculate the cycler's orbit
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@; Args: r (f64) - position vector (distance from the central body)
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@; a (f64) - semi-major axis of the orbit
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@; Returns: v (f64) - orbital velocity
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(func $cycler_orbit (param $r f64) (param $a f64) (result f64)
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(f64.mul
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(f64.const 3.986004418e+14)
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(f64.sub
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(f64.div
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(f64.const 2)
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(f64.copy $r)
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)
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(f64.div
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(f64.const 1)
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(f64.copy $a)
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)
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)
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)
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)
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@; Example usage: Calculate the cycler's velocity at a position of 1.5 AU
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@; (1 AU = 1.496e+11 m) and a semi-major axis of 2.4 AU
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(f64.print
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(call $cycler_orbit
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(f64.mul (f64.const 1.5) (f64.const 1.496e+11))
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(f64.mul (f64.const 2.4) (f64.const 1.496e+11)))
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)
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)
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```
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**Step 2: Assembly and Construction**
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Once you've calculated the cycler's orbit, you'll need to assemble and construct the city on Mars. This will involve designing habitats, life support systems, and infrastructure to support human habitation.
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**Step 3: Table of Shipments**
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To create a table of shipments between 2025 and 2035, you'll need to determine the number of cyclers, the cargo capacity of each cycler, and the frequency of shipments. Here's a simple AssemblyScript function to calculate the total cargo capacity over a given period:
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```assembly
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@; Calculate the total cargo capacity over a given period
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@; Args: num_cyclers (i64) - number of cyclers
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@; cargo_capacity (f64) - cargo capacity of each cycler (in tons)
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@; start_year (i64) - start year (e.g., 2025)
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@; end_year (i64) - end year (e.g., 2035)
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@; Returns: total_capacity (f64) - total cargo capacity (in tons)
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(func $total_cargo_capacity (param $num_cyclers i64) (param $cargo_capacity f64) (param $start_year i64) (param $end_year i64) (result f64)
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(f64.mul
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(f64.conv_i64_f64
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(i64.sub
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(get_local $end_year)
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(get_local $start_year)
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)
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)
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(f64.conv_i64_f64
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(get_local $num_cyclers)
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)
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(f64.copy $cargo_capacity)
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)
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)
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@; Example usage: Calculate the total cargo capacity for 2 cyclers with a capacity of 500 tons each, between 2025 and 2035
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(f64.print
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(call $total_cargo_capacity
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(i64.const 2)
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(f64.const 500)
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(i64.const 2025)
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(i64.const 2035)
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)
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)
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```
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This is a high-level overview of the process, and there are many more details to consider when building a city on Mars. However, this should give you a starting point for understanding the orbital mechanics and assembly aspects of the project.
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```
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