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The mixture ratio of rocket propellants refers to the ratio of oxidizer to fuel in a rocket engine. It is an important parameter that determines the performance and efficiency of the engine. The specific mixture ratio can vary depending on the type of propellants used and the design requirements of the rocket.
The atomic ratio in this salt is 1:1. The mass ratio is 22.999:35.457 of sodium to chlorine, the ratio of the atomic weights of sodium and chlorine.
In sodium chloride, the ratio is 1/1.
The lowest whole number mass ratio of copper that combines with a given mass of chlorine is 1:1, meaning each mole of copper combines with one mole of chlorine. This corresponds to the compound copper (I) chloride, where the mass ratio would be 63.5 grams of copper to 35.5 grams of chlorine.
the ratio of the mean diameter of the body of a rocket or missile to its length
The ratio of aluminum to chlorine in aluminum chloride is 1:3. This means for every one atom of aluminum, there are three atoms of chlorine in the compound.
The ratio of brake power output to power input
The ratio mass of chlorine/mass of sodium is 1,5.
The chemical ratio of carbon to chlorine in carbon tetrachloride (CCl4) is 1:4. The chemical ratio of carbon to fluorine in carbon tetrafluoride (CF4) is also 1:4.
The ratio of lithium to chlorine in lithium chloride is 1:1. This means that one lithium ion combines with one chloride ion to form a stable compound.
You would need to add 1.5 ounces of chlorine to achieve the 1:10 ratio in 15 ounces of water.
The ratio of sodium atoms to chlorine atoms in sodium chloride (NaCl) is 1:1. This means there is one sodium atom for every one chlorine atom in a molecule of sodium chloride.