> For the complete documentation index, see [llms.txt](https://fdrtn.gitbook.io/the-core-network/llms.txt). Markdown versions of documentation pages are available by appending `.md` to page URLs; this page is available as [Markdown](https://fdrtn.gitbook.io/the-core-network/the-core-universe/interstellar-infrastructure/ion-propulsion/construction-details.md).

# Construction Details

The construction of the Ion Propulsion platform on Mars represents a major advancement in space technology, as it introduces argon as the primary fuel for the first time. This shift to argon powers the entire system, providing sustained thrust and enabling long-distance missions. The launchpad integrates multiple systems that work together to ensure efficient fueling, energy distribution, and thermal management, all tailored to the specific demands of the Martian environment. Built with advanced materials and precision engineering, the platform is capable of handling the complexities of interplanetary launches.

Operationally, the platform brings together robust external support systems like cooling mechanisms and stabilization structures, ensuring smooth and secure launches. The introduction of argon as fuel increases efficiency, allowing for longer missions beyond Mars to Jupiter, Saturn, and their moons. This platform represents a critical step in space exploration, facilitating humanity’s journey deeper into the solar system with a more sustainable and advanced propulsion system.\
\
**Global Yield: 10%** \
\
**A 10% share of the resources produced by districts accessed via the Ion Propulsion Rocket will be allocated to the builders and maintainers of the launchpad.**\ <br>

<table data-full-width="true"><thead><tr><th>Id</th><th width="194">Component Name</th><th width="134">Code Name</th><th width="392">Description</th><th width="158">Section</th><th width="141">External Component</th><th width="199">Internal Components</th><th width="116">Fuel</th><th width="145">Cosmic Yield</th><th width="160">External Mat.</th><th width="126">Internal Mat.</th><th width="122">Fuel</th></tr></thead><tbody><tr><td>4001</td><td>Fueling Umbilical Assembly</td><td>FUA</td><td>Provides fuel to the rocket through retractable arms.</td><td>Inner Circle</td><td>Aluminum</td><td>Silicon</td><td>Argon</td><td>1.90%</td><td>12,000,000</td><td>6,000,000</td><td>6,000,000</td></tr><tr><td>4002</td><td>Power Distribution Hub</td><td>PDHUB</td><td>Central unit distributing power to the rocket and other launch systems.</td><td>Inner Circle</td><td>Aluminum</td><td>Silicon</td><td>Helium-3</td><td>1.60%</td><td>10,500,000</td><td>5,250,000</td><td>5,250,000</td></tr><tr><td>4003</td><td>Thermal Management System</td><td>TMS</td><td>Regulates temperature during pre-launch, ensuring systems remain within operational limits.</td><td>Inner Circle</td><td>Aluminum</td><td>Carbon</td><td>Helium-3</td><td>1.40%</td><td>9,750,000</td><td>4,875,000</td><td>4,875,000</td></tr><tr><td>4004</td><td>Rocket Gantry</td><td>RGANTRY</td><td>Support structure that stabilizes the rocket vertically, retracts during launch.</td><td>Inner Circle</td><td>Titanium</td><td>Carbon</td><td>Helium-3</td><td>2.00%</td><td>12,750,000</td><td>6,375,000</td><td>6,375,000</td></tr><tr><td>4005</td><td>Propellant Loading Dock</td><td>PLDOCK</td><td>Facilitates the loading of propellant into the rocket tanks.</td><td>Inner Circle</td><td>Aluminum</td><td>Carbon</td><td>Argon</td><td>1.90%</td><td>12,000,000</td><td>6,000,000</td><td>6,000,000</td></tr><tr><td>4006</td><td>Ignition Sequence Controller</td><td>IGCTRL</td><td>Manages the sequence of ignition commands for a smooth launch process.</td><td>Inner Circle</td><td>Silicon</td><td>Carbon</td><td>Helium-3</td><td>2.20%</td><td>13,500,000</td><td>6,750,000</td><td>6,750,000</td></tr><tr><td>4007</td><td>Command Interface Terminal</td><td>CINTERM</td><td>The central command interface for controlling the launch procedures.</td><td>Inner Circle</td><td>Silicon</td><td>Aluminum</td><td>Helium-3</td><td>1.70%</td><td>11,250,000</td><td>5,625,000</td><td>5,625,000</td></tr><tr><td>4008</td><td>Rocket Cooling Ducts</td><td>COOLDUCT</td><td>Channels that direct cool air or liquid to the rocket engines before and during launch.</td><td>Inner Circle</td><td>Aluminum</td><td>Carbon</td><td>Helium-3</td><td>1.40%</td><td>9,750,000</td><td>4,875,000</td><td>4,875,000</td></tr><tr><td>4009</td><td>Launch Clamps</td><td>LCLAMPS</td><td>Mechanical clamps that hold the rocket securely on the platform until ignition.</td><td>Inner Circle</td><td>Titanium</td><td>Carbon</td><td>Helium-3</td><td>1.70%</td><td>11,250,000</td><td>5,625,000</td><td>5,625,000</td></tr><tr><td>4010</td><td>Stabilization Gyroscopes</td><td>STABGYRO</td><td>Gyroscopes that help maintain the rocket's stability during initial lift-off.</td><td>Inner Circle</td><td>Titanium</td><td>Silicon</td><td>Helium-3</td><td>2.00%</td><td>12,750,000</td><td>6,375,000</td><td>6,375,000</td></tr><tr><td>4011</td><td>Maintenance Bay I</td><td>MBAY I</td><td>Maintenance bay for housing tools, equipment, or vehicles.</td><td>Outer Circle</td><td>Aluminum</td><td>Carbon</td><td>Helium-3</td><td>1.60%</td><td>10,500,000</td><td>5,250,000</td><td>5,250,000</td></tr><tr><td>4012</td><td>Maintenance Bay II</td><td>MBAY II</td><td>Additional maintenance bay for redundancy and accessibility.</td><td>Outer Circle</td><td>Aluminum</td><td>Carbon</td><td>Helium-3</td><td>1.60%</td><td>10,500,000</td><td>5,250,000</td><td>5,250,000</td></tr><tr><td>4013</td><td>Exhaust Venting System</td><td>EXVENT</td><td>Directs exhaust gases away from the platform during rocket ignition.</td><td>Outer Circle</td><td>Carbon</td><td>Aluminum</td><td>Helium-3</td><td>1.70%</td><td>22,500,000</td><td>11,250,000</td><td>5,625,000</td></tr><tr><td>4014</td><td>Cooling Channels</td><td>COOLCHAN</td><td>Network of channels that circulates coolant to manage heat across the platform.</td><td>Outer Circle</td><td>Aluminum</td><td>Carbon</td><td>Helium-3</td><td>1.40%</td><td>19,500,000</td><td>9,750,000</td><td>4,875,000</td></tr><tr><td>4015</td><td>Launch Lighting Array</td><td>LLA</td><td>High-intensity lights that illuminate the launch area.</td><td>Outer Circle</td><td>Aluminum</td><td>Silicon</td><td>Helium-3</td><td>1.10%</td><td>16,500,000</td><td>8,250,000</td><td>4,125,000</td></tr><tr><td>4016</td><td>Safety Barrier Mechanisms</td><td>SBMECH</td><td>Deploys physical barriers to protect nearby areas during launch.</td><td>Outer Circle</td><td>Carbon</td><td>Aluminum</td><td>Helium-3</td><td>1.40%</td><td>19,500,000</td><td>9,750,000</td><td>4,875,000</td></tr><tr><td>4017</td><td>Environmental Control Systems</td><td>ENVCTRL</td><td>Controls environmental conditions, such as temperature and pressure, across the platform.</td><td>Outer Circle</td><td>Aluminum</td><td>Carbon</td><td>Helium-3</td><td>1.90%</td><td>19,500,000</td><td>9,750,000</td><td>4,875,000</td></tr><tr><td>4018</td><td>Emergency Ejection Mechanism</td><td>EJEMECH</td><td>System designed to safely eject personnel or equipment in case of emergencies.</td><td>Outer Circle</td><td>Titanium</td><td>Carbon</td><td>Helium-3</td><td>2.80%</td><td>28,500,000</td><td>14,250,000</td><td>7,125,000</td></tr><tr><td>4019</td><td>Fuel Transfer Pipelines</td><td>FTPIPES</td><td>Pipelines that transfer fuel from storage tanks to the rocket.</td><td>Outer Circle</td><td>Aluminum</td><td>Silicon</td><td>Argon</td><td>2.40%</td><td>24,000,000</td><td>12,000,000</td><td>6,000,000</td></tr><tr><td>4020</td><td>Emergency Power Generators</td><td>EPGEN</td><td>Backup power generators that supply energy in case of power failure.</td><td>Outer Circle</td><td>Aluminum</td><td>Carbon</td><td>Helium-3</td><td>2.20%</td><td>22,500,000</td><td>11,250,000</td><td>5,625,000</td></tr><tr><td>4021</td><td>Secure Access Gates</td><td>SACCGATE</td><td>Gates that control access to the platform, ensuring only authorized personnel are present.</td><td>Outer Circle</td><td>Aluminum</td><td>Carbon</td><td>Helium-3</td><td>1.90%</td><td>19,500,000</td><td>9,750,000</td><td>4,875,000</td></tr><tr><td>4022</td><td>Crew Preparation Room</td><td>CREWPREP</td><td>Dedicated room where the crew prepares before launch, including final checks and suit-up.</td><td>Outer Circle</td><td>Aluminum</td><td>Carbon</td><td>Helium-3</td><td>2.40%</td><td>24,000,000</td><td>12,000,000</td><td>6,000,000</td></tr><tr><td>4023</td><td>Exhaust Ventilation System</td><td>EXVENTALT</td><td>Alternative exhaust system that provides additional venting capacity during intense launches.</td><td>Outer Circle</td><td>Carbon</td><td>Silicon</td><td>Helium-3</td><td>2.20%</td><td>22,500,000</td><td>11,250,000</td><td>5,625,000</td></tr><tr><td>4024</td><td>Auxiliary Cooling Channels</td><td>AUXCOOLCHAN</td><td>Backup coolant channels that activate if primary systems overheat during extended launch phases.</td><td>Outer Circle</td><td>Aluminum</td><td>Carbon</td><td>Helium-3</td><td>1.90%</td><td>19,500,000</td><td>9,750,000</td><td>4,875,000</td></tr><tr><td>4025</td><td>Emergency Lighting Array</td><td>EMERLLA</td><td>Secondary lighting array that activates during emergency launch procedures, ensuring visibility.</td><td>Outer Circle</td><td>Aluminum</td><td>Silicon</td><td>Helium-3</td><td>1.50%</td><td>16,500,000</td><td>8,250,000</td><td>4,125,000</td></tr><tr><td>4026</td><td>Shock Absorption System</td><td>SHOCKABS</td><td>Absorbs vibrations and shocks during rocket ignition, protecting both rocket and platform.</td><td>Outer Circle</td><td>Carbon</td><td>Silicon</td><td>Helium-3</td><td>2.40%</td><td>24,000,000</td><td>12,000,000</td><td>6,000,000</td></tr><tr><td>4027</td><td>Retractable Service Arms</td><td>RSARMS</td><td>Arms that provide service and connections to the rocket, retracting before launch.</td><td>Outer Circle</td><td>Titanium</td><td>Aluminum</td><td>Helium-3</td><td>2.20%</td><td>22,500,000</td><td>11,250,000</td><td>5,625,000</td></tr><tr><td>4028</td><td>Platform Integrity Monitors</td><td>PLATMON</td><td>Sensors that monitor the structural integrity of the platform during launch.</td><td>Outer Circle</td><td>Aluminum</td><td>Silicon</td><td>Helium-3</td><td>2.10%</td><td>21,000,000</td><td>10,500,000</td><td>5,250,000</td></tr><tr><td>4029</td><td>Central Launch Stabilizer</td><td>CLS</td><td>Central structure that holds the rocket in place during pre-launch and initial ignition.</td><td>Inner Circle</td><td>Titanium</td><td>Carbon</td><td>Helium-3</td><td>2.70%</td><td>27,000,000</td><td>13,500,000</td><td>6,750,000</td></tr><tr><td>4030</td><td>Entrance Track</td><td>INTRANS</td><td>Pathway used for the entrance of personnel and cargo onto the platform.</td><td>Outer Circle</td><td>Aluminum</td><td>Carbon</td><td>Helium-3</td><td>1.80%</td><td>18,000,000</td><td>9,000,000</td><td>4,500,000</td></tr><tr><td>4031</td><td>Exit Track</td><td>EXIT</td><td>Pathway used for the exit of personnel and cargo from the platform.</td><td>Outer Circle</td><td>Aluminum</td><td>Carbon</td><td>Helium-3</td><td>1.80%</td><td>18,000,000</td><td>9,000,000</td><td>4,500,000</td></tr><tr><td>4032</td><td>Docking Module</td><td>DOCKMOD</td><td>Interface for docking with other spacecraft or space stations.</td><td>Nose Cone</td><td>Aluminum</td><td>Titanium</td><td>Helium-3</td><td>2.90%</td><td>19,500,000</td><td>9,750,000</td><td>9,750,000</td></tr><tr><td>4033</td><td>Payload Bay</td><td>PAYLOAD</td><td>Compartment for carrying cargo or scientific instruments.</td><td>Nose Cone</td><td>Aluminum</td><td>Titanium</td><td>Helium-3</td><td>2.30%</td><td>18,000,000</td><td>9,000,000</td><td>9,000,000</td></tr><tr><td>4034</td><td>Instrument Panel</td><td>INSPAN</td><td>Displays all the crucial data for the crew or autonomous systems.</td><td>Nose Cone</td><td>Silicon</td><td>REE</td><td>Helium-3</td><td>2.10%</td><td>16,500,000</td><td>8,250,000</td><td>8,250,000</td></tr><tr><td>4035</td><td>Navigation Module</td><td>NAVMOD</td><td>Controls the direction and trajectory of the rocket.</td><td>Nose Cone</td><td>Silicon</td><td>REE</td><td>Helium-3</td><td>2.40%</td><td>19,500,000</td><td>9,750,000</td><td>9,750,000</td></tr><tr><td>4036</td><td>Communication Array</td><td>COMARRAY</td><td>Ensures long-range communication with mission control.</td><td>Upper Body</td><td>Titanium</td><td>Silicon</td><td>Helium-3</td><td>2.60%</td><td>21,000,000</td><td>10,500,000</td><td>10,500,000</td></tr><tr><td>4037</td><td>Avionics Suite</td><td>AVSUITE</td><td>The suite of electronic systems for flight control and monitoring.</td><td>Upper Body</td><td>Silicon</td><td>REE</td><td>Helium-3</td><td>2.70%</td><td>22,500,000</td><td>11,250,000</td><td>11,250,000</td></tr><tr><td>4038</td><td>Life Support System</td><td>LIFESUP</td><td>Ensures the survival of the crew by providing air, water, and temperature control.</td><td>Midsection</td><td>Carbon</td><td>Silicon</td><td>Helium-3</td><td>2.90%</td><td>24,000,000</td><td>12,000,000</td><td>12,000,000</td></tr><tr><td>4039</td><td>Thermal Control System</td><td>TCSYS</td><td>Regulates the temperature within the propulsion system and other critical components.</td><td>Midsection</td><td>Carbon</td><td>REE</td><td>Helium-3</td><td>2.40%</td><td>19,500,000</td><td>9,750,000</td><td>9,750,000</td></tr><tr><td>4040</td><td>Reactor Core</td><td>REACTCORE</td><td>Generates the primary power for the ion propulsion system.</td><td>Midsection</td><td>Silicon</td><td>Carbon</td><td>Argon</td><td>3.30%</td><td>28,500,000</td><td>14,250,000</td><td>14,250,000</td></tr><tr><td>4041</td><td>Argon Fuel Tanks</td><td>AFTANK</td><td>Storage tanks for argon, the primary fuel for the ion propulsion system.</td><td>Engine Section</td><td>Carbon</td><td>REE</td><td>Argon</td><td>2.90%</td><td>24,000,000</td><td>12,000,000</td><td>12,000,000</td></tr><tr><td>4042</td><td>Propellant Ionizer</td><td>PROPION</td><td>Device that ionizes the argon fuel for the propulsion system.</td><td>Engine Section</td><td>Silicon</td><td>REE</td><td>Argon</td><td>3.00%</td><td>25,500,000</td><td>12,750,000</td><td>12,750,000</td></tr><tr><td>4043</td><td>Ion Accelerator</td><td>IONACCEL</td><td>Accelerates the ionized propellant to create thrust.</td><td>Engine Section</td><td>Titanium</td><td>REE</td><td>Argon</td><td>3.00%</td><td>25,500,000</td><td>12,750,000</td><td>12,750,000</td></tr><tr><td>4044</td><td>Main Engine Assembly</td><td>MENGINE</td><td>Primary thrust-providing engines for propulsion.</td><td>Engine Section</td><td>Titanium</td><td>Silicon</td><td>Argon</td><td>3.30%</td><td>28,500,000</td><td>14,250,000</td><td>14,250,000</td></tr><tr><td>4045</td><td>Propulsion Gimbal System I</td><td>PROPGBL I</td><td>Allows the engines to pivot and steer the spacecraft.</td><td>Engine Section</td><td>Titanium</td><td>Carbon</td><td>Argon</td><td>2.70%</td><td>22,500,000</td><td>11,250,000</td><td>11,250,000</td></tr><tr><td>4046</td><td>Propulsion Gimbal System II</td><td>PROPGBL II</td><td>Allows the engines to pivot and steer the spacecraft.</td><td>Engine Section</td><td>Titanium</td><td>Carbon</td><td>Argon</td><td>2.70%</td><td>22,500,000</td><td>11,250,000</td><td>11,250,000</td></tr></tbody></table>


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