Begin from the original form of torture and become immortal
Chapter 1702: The Battle between Technology and Biology
Chapter 1702: The Battle between Technology and Biology
Secondary krypton gold has an extremely high melting point and thermal conductivity, and can maintain stable physical properties in extremely high temperature environments.
In the MK space weapon, it serves as the core material of the launch device and is responsible for withstanding the huge energy output generated when the plasma jet is launched.
A plasma jet is an energy beam composed of high-temperature, high-energy plasma. Its temperature can reach millions or even tens of millions of degrees Celsius and its energy density is extremely high.
When launching a plasma jet, the launch device needs to withstand huge thermal and mechanical stresses.
The Ark Arc cold nuclear fusion reactor provides a continuous source of energy for MK space weapons. Although it is cold nuclear fusion, the release of energy still follows the basic laws of thermal effect and heat transfer.
As the key component that bears the load and undertakes this huge energy output, the secondary krypton gold launch device is subjected to unimaginable high pressure and high heat.
At the moment the plasma jet is launched, the temperature on the surface of the launch device will rise sharply, reaching thousands of degrees Celsius or even higher.
Fortunately, the metal properties of secondary krypton gold are extraordinary, and it has a low metal fatigue value. Metal fatigue refers to the phenomenon that materials produce cracks or breakage after a certain number of cycles under alternating stress.
After the secondary krypton gold reaches the critical point, as long as it is cooled in time, its performance can be quickly restored and put into use again.
In order to deal with possible damage to the launch device, Tony prepared five sets of launch devices.
"Start the replacement procedure and automatically replace the launcher."
Jarvis followed Tony's instructions and quickly started the replacement procedure.
The robotic arm inside the MK space weapon began to operate precisely, slowly removing the damaged launcher, and then taking out a new launcher from the storage compartment for installation.
The whole process was smooth and efficient, and every action was precisely calculated and controlled to ensure that it would not affect other components of the MK space weapon.
The launch device will withstand a huge energy impact and generate extremely high heat when firing a plasma jet, so Tony designed an active circulation liquid cooling system specifically for the MK space weapon.
This system is mainly composed of high-performance coolant, micro circulation pump, heat dissipation pipes and efficient heat exchangers.
The coolant is a specially developed nanofluid with extremely high thermal conductivity and specific heat capacity, which can absorb a large amount of heat in a short time.
When the launch device is operating normally, the micro circulation pump will continue to work, pushing the coolant to circulate in the heat dissipation pipe.
The heat dissipation pipes are tightly fitted to the key heat-generating parts of the launch device, such as the plasma generation chamber, energy conduction lines, etc. When the coolant flows through these parts, it will quickly absorb the heat and take it away.
The coolant then enters the heat exchanger, carrying the heat.
The heat exchanger uses advanced thermoelectric conversion technology, which can convert the heat energy in the coolant into electrical energy. Part of the electrical energy can be fed back to the energy system of the MK space weapon to improve energy utilization efficiency; the other part is used to assist the cooling process.
At the same time, the heat exchanger is also connected to the external cooling fins. The cooling fins are made of special materials and structural design, have a large heat dissipation area, and can quickly dissipate the remaining heat into the surrounding space environment.
When the launcher overheats and is overloaded, the active circulation liquid cooling system will immediately increase its working intensity. The micro-circulation pump will increase the speed of the coolant circulation to ensure that it can absorb and remove heat faster. The heat exchanger will also operate at full capacity to improve the efficiency of thermoelectric conversion and accelerate the dissipation of heat. This active circulation liquid cooling system can effectively reduce the temperature of the launcher in a short period of time and prevent it from being damaged by overheating.
In addition to the active circulation liquid cooling system, Tony also embedded phase change materials in key parts of the launcher.
Phase change material is a substance that can undergo phase change (such as from solid to liquid or from liquid to gas) at a specific temperature and absorb or release a large amount of heat.
The phase change material selected by Tony has a suitable phase change temperature. When the temperature of the launch device rises to close to its phase change temperature, the phase change material will begin to undergo phase change and absorb a large amount of heat, thereby playing a role in buffering the temperature rise.
For example, when a plasma jet is launched, the temperature of the launch device will rise sharply, and the phase change material will quickly change from solid to liquid, absorbing a large amount of latent heat, thereby slowing down the temperature rise of the launch device.
When the launch process is completed and the temperature of the launch device gradually decreases, the phase change material will change from liquid back to solid, releasing the heat previously absorbed.
This released heat can be further dissipated through an active circulation liquid cooling system.
The phase change material assisted cooling system and the active circulation liquid cooling system work together to form an efficient cooling system that can better cope with the overheating and overload of the launch device.
In the space environment, since there is no atmosphere to hinder the heat dissipation, radiation heat dissipation is a very effective way of heat dissipation.
Tony made full use of this feature and carried out a careful radiation heat dissipation design for the launch device of the MK space weapon.
The outer shell of the launch device is made of high-emissivity material, which can efficiently radiate internal heat into the surrounding space environment in the form of electromagnetic waves.
The surface of the shell has also been specially treated to form a tiny concave-convex structure, which increases the heat dissipation area and further improves the radiation heat dissipation efficiency.
In addition, Tony also set up some heat dissipation radiation panels around the launch device.
These radiation panels are connected to the transmitting device through heat pipes, which can quickly transfer the heat from the transmitting device to the radiation panels and then dissipate it through radiation.
The heat dissipation radiation panel adopts a special shape and angle design, which can maximize the use of the low temperature environment in space and improve the heat dissipation effect.
Although the space environment is special, the temperature in the area facing away from the sun is extremely low, close to absolute zero. Tony cleverly used this low temperature environment to assist in cooling the launch device.
In the design of the MK space weapon, some heat dissipation channels are directly connected to the external space environment. When the launch device overheats, these heat dissipation channels will open to allow the hot air or coolant inside to exchange heat with the external low-temperature space environment.
For example, a portion of the coolant in an active circulation liquid cooling system can be directly exposed to space through a heat dissipation channel, rapidly cooled by the low temperature in space, and then flow back into the system for continued circulation.
At the same time, Tony also set up some deployable cooling fins around the launch device. These cooling fins can be folded up at ordinary times to reduce the impact on the overall structure of the MK space weapon.
(End of this chapter)
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