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List of contents in this article:

• 1,Advantages of liquid hydrogen as rocket fuel
• 2, Which liquid hydrogen liquid oxygen engine is used in the new generation launch vehicle series
• 3、The rocket engine used by the Saturn 5 rocket is
• 4, What are the advantages of liquid hydrogen as aviation fuel
• 5, What are the advantages and disadvantages of the kerosene engine of the carrier rocket compared with the liquid hydrogen liquid oxygen engine?
• 6, What are the advantages of using liquid hydrogen as aviation fuel

Advantages of liquid hydrogen as rocket fuel

Liquid hydrogen has a large calorific value. When the same mass, it emits more heat than other fuel combustion, which can make the rocket achieve a large initial speed, so liquid hydrogen should be selected as the fuel of the rocket engine. Chemically speaking, the energy density (energy per unit weight) of liquid hydrogen is high.

So liquid hydrogen is used as a propellant. Therefore, hydrogen has the advantage of being a fuel: it burns a lot of heat, and the product is pollution-free water;It can be made of water, and water can be generated by combustion, which can be regenerated.

High propulsion performance: Liquid hydrogen has excellent propulsion performance. The combustion combination of liquid hydrogen and liquid oxygen produces a very high exhaust speed, which is required to propel the rocket. High exhaust speed means that the rocket can break away from the earth's gravity at a higher speed, enter orbit and explore space.

The reasons why liquid hydrogen is used as rocket fuel are as follows: liquid hydrogen has a high calorific value and can release more heat when it completely burns the same mass of hydrogen. Liquid hydrogen is an ideal energy material that can be used to obtain great energy efficiency and low-cost energy.

The advantage of liquid hydrogen is that it is completely pollution-free, and the product is water, and it has greater thrust and better economy. Liquid hydrogen is currently being studied in various countries, and its advantages are good safety and environmental protection.There is a kind of fuel agent called "malone" that is also commonly used, but it is both toxic and corrosive.

Which liquid hydrogen liquid oxygen engine is used in the new generation launch vehicle series

1. The rocket engine used in Saturn 5 rocket is the Saturn rocket engine (S-ICD S). The Saturn rocket engine is a high-performance liquid oxygen/liquid hydrogen rocket engine, which is the main power source used by the National Aeronautics and Space Administration (NASA) for the Saturn V rocket.

2. Its core stage is based on the design of the Long March 7 launch vehicle and the Long March 3A series. The first sub-stage of the rocket adopts two YF-100 liquid oxygen kerosene engines, and the second sub-stage of the rocket adopts the YF-75 liquid hydrogen liquid oxygen engine (dual machine).

3. The first sub-stage of the H2A rocket uses the LE-7A liquid hydrogen-liquid-oxygen main engine with a thrust of 110 tons, and the second sub-stage uses the LE-5B liquid hydrogen-liquid-oxygen main engine with a thrust of 137 kN.

4. The Chang'e-5 rocket uses a liquid-oxygen and liquid-hydrogen engine for the first-class core and the second-class core. Booster (first separation), using liquid oxygen + kerosene.

5. In terms of the engine, the SLS launch vehicle is equipped with a strong RS-25 liquid hydrogen liquid oxygen engine, but its cost is so high that a single launch mission of "Falcon 9" can be purchased! And one rocket needs to carry four, which can completely buy a "heavy Falcon" rocket.

The rocket engine used in the Saturn V rocket is

In order to optimize the configuration of Saturn V, they adopted the F rocket engine and the new J2 rocket engine. The combination of the two lays the hardware foundation for its successful launch, and liquid hydrogen liquid oxygen propellant was used during the launch process, which also It laid the driving foundation for the successful launch of Mars 5.

F-1 rocket engine The world's largest thrust single-chamber liquid rocket engine developed by the United States is used for the Saturn 5 rocket, with a single thrust of 700 tons, using kerosene as fuel, and liquid oxygen as an oxidizing agent.

F-1 rocket engine is a kerosene liquid oxygen engine designed and manufactured by Rockdain in the United States, which is used for the first stage of Saturn V. F-1 is the single-nezzle liquid engine with the largest thrust in use.

Saturn 5 is currently the world's largest practical rocket, with a total weight of 3,038 tons, and the total thrust of the first-class engine is as high as 3,408 tons, which is equivalent to the total thrust of dozens of large passenger aircraft. The designer of Saturn 5 is Von Braun, a crazy scientist from Germany.

What are the advantages of liquid hydrogen as aviation fuel

1. The advantages of using liquid hydrogen as aviation fuel are: liquid hydrogen has high energy density, zero emissions, fast filling, suitable for long-range flights, energy diversity and renewable energy matching, etc.

2. The biggest advantage is that its combustion product is water and does not pollute the environment. More heat is released during combustion, about 3 times that of gasoline of the same mass, 9 times that of alcohol, and 5 times that of coke. As an energy source, hydrogen has advantages that other energy sources do not have and is widely used.

3. The advantages of liquid hydrogen as an aviation fuel are mainly manifested in the following aspects: High energy density: Liquid hydrogen has a high energy density, which means that liquid hydrogen per unit mass contains more energy, so it can provide longer range and greater thrust.

What are the advantages and disadvantages of the kerosene engine of the carrier rocket compared with the liquid hydrogen liquid oxygen engine?

1. The most obvious advantage of liquid oxygen kerosene engine is that it can be stored at room temperature. Compared with liquid hydrogen, hydrogen storage is safe and convenient, with high thrust, but cannot be reused. But as the first-stage fuel of the rocket, the situation is not good. This high-pressure posture is the main reason.

2. The specific calorific value of hydrogen must be greater than that of kerosene. After all, H2 is the lightest monomer. It can be said that liquid hydrogen liquid oxygen propellant consumes the same mass and provides the most energy! But if you put the thrust on the larger ratio, that belongs to the power size, just like saying which motor of the car has more horsepower.

3. Liquid engines can store propellants: kerosene, nitric acid, etc.Low-temperature propellant: liquid hydrogen, liquid oxygen, etc. Liquid engine two-component propellant single-component propellant oxidant: liquid oxygen, nitric acid, hydrogen peroxide, nitrogen tetraoxide, etc. Combustion agents: liquid hydrogen, kerosene, alcohol, dimethyl, methylene, etc.

4. The third stage of China's "Long March" No. 3 carrier rocket engine adopts liquid hydrogen and liquid oxygen as propellants, becoming the third country in the world to master the technology of controlling liquid hydrogen. Hydrogen is the most active of all elements, and it is extremely difficult to control the combustion of liquid hydrogen.

What are the advantages of using liquid hydrogen as aviation fuel

1. The advantages of liquid hydrogen as an aviation fuel are mainly manifested in the following aspects: high energy density: liquidHydrogen has a high energy density, which means that liquid hydrogen per unit mass contains more energy, so it can provide a longer range and greater thrust.

2. The advantages of using liquid hydrogen as aviation fuel are: liquid hydrogen has high energy density, zero emissions, fast filling, suitable for long-range flights, energy diversity and renewable energy matching, etc.

3. It can be made with widespread water as raw material. The biggest advantage is that its combustion product is water, which does not pollute the environment. More heat is released during combustion, about 3 times that of gasoline of the same mass, 9 times that of alcohol, and 5 times that of coke.