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.

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