The relationship between the enthalpy (\(H\)) and internal energy (\(U\)) can be given by the following equation: \[ \Delta H = \Delta U + \Delta nRT \] Where: - \(\Delta H\) is the change in enthalpy (given as -2546 kJ/mol), - \(\Delta n\) is the change in the number of moles of gas in the reaction,
- \(R\) is the gas constant (\(8.314 \, J \, mol^{-1} \, K^{-1}\)),
- \(T\) is the temperature in Kelvin (298 K at 25°C). In the case of combustion, the combustion products (carbon dioxide and water) usually result in no change in the number of moles of gas (\(\Delta n = 0\)).
Therefore, the internal energy change \(\Delta U\) is equal to the enthalpy change \(\Delta H\): \[ \Delta U = \Delta H \] Hence, the internal energy change for the reaction is -2544.8 kJ/mol.
A gaseous fuel mixture comprising 3 moles of methane and 2 moles of ammonia is combusted in \( X \) moles of pure oxygen in stoichiometric amount. Assuming complete combustion, with only \( {CO}_2 \), \( {H}_2{O} \), and \( {N}_2 \) in the product gases, the value of \( X \) is ____________. \[ 3 \, {CH}_4 + 2 \, {NH}_3 + X \, {O}_2 \rightarrow {Products (CO}_2, \, {H}_2{O}, \, {N}_2{)} \]
An ideal two-stage rocket has identical specific impulse and structural coefficient for its two stages. For an optimized rocket, the two stages have identical payload ratio as well. The payload is 2 tons and the initial mass of the rocket is 200 tons. The mass of the second stage of the rocket (including the final payload mass) is ___________ tons.
A solid cylinder of mass 2 kg and radius 0.2 m is rotating about its own axis without friction with angular velocity 5 rad/s. A particle of mass 1 kg moving with a velocity of 5 m/s strikes the cylinder and sticks to it as shown in figure.
The angular velocity of the system after the particle sticks to it will be: