146357 A \(5000 \mathrm{~kg}\) rocket is set for vertical firing. The exhaust speed is \(800 \mathrm{~ms}^{-1}\). To give an initial upward acceleration of \(20 \mathrm{~m} / \mathrm{s}^{2}\), the amount of gas ejected per second to supply the needed thrust will be \(\left(\mathrm{g}=10 \mathrm{~ms}^{-2}\right)\)
146359 A rocket of mass \(1000 \mathrm{~kg}\) is to be projected vertically upwards. The gases are exhausted vertically downwards with velocity \(100 \mathrm{~ms}^{-1}\) with respect to the rocket. What is the minimum rate of burning of fuel, so as to just lift the rocket upwards of fuel, so as to just lift the rocket upwards against, the gravitational attraction? (Take \(g=10 \mathrm{~ms}^{-2}\) )
146357 A \(5000 \mathrm{~kg}\) rocket is set for vertical firing. The exhaust speed is \(800 \mathrm{~ms}^{-1}\). To give an initial upward acceleration of \(20 \mathrm{~m} / \mathrm{s}^{2}\), the amount of gas ejected per second to supply the needed thrust will be \(\left(\mathrm{g}=10 \mathrm{~ms}^{-2}\right)\)
146359 A rocket of mass \(1000 \mathrm{~kg}\) is to be projected vertically upwards. The gases are exhausted vertically downwards with velocity \(100 \mathrm{~ms}^{-1}\) with respect to the rocket. What is the minimum rate of burning of fuel, so as to just lift the rocket upwards of fuel, so as to just lift the rocket upwards against, the gravitational attraction? (Take \(g=10 \mathrm{~ms}^{-2}\) )
146357 A \(5000 \mathrm{~kg}\) rocket is set for vertical firing. The exhaust speed is \(800 \mathrm{~ms}^{-1}\). To give an initial upward acceleration of \(20 \mathrm{~m} / \mathrm{s}^{2}\), the amount of gas ejected per second to supply the needed thrust will be \(\left(\mathrm{g}=10 \mathrm{~ms}^{-2}\right)\)
146359 A rocket of mass \(1000 \mathrm{~kg}\) is to be projected vertically upwards. The gases are exhausted vertically downwards with velocity \(100 \mathrm{~ms}^{-1}\) with respect to the rocket. What is the minimum rate of burning of fuel, so as to just lift the rocket upwards of fuel, so as to just lift the rocket upwards against, the gravitational attraction? (Take \(g=10 \mathrm{~ms}^{-2}\) )
146357 A \(5000 \mathrm{~kg}\) rocket is set for vertical firing. The exhaust speed is \(800 \mathrm{~ms}^{-1}\). To give an initial upward acceleration of \(20 \mathrm{~m} / \mathrm{s}^{2}\), the amount of gas ejected per second to supply the needed thrust will be \(\left(\mathrm{g}=10 \mathrm{~ms}^{-2}\right)\)
146359 A rocket of mass \(1000 \mathrm{~kg}\) is to be projected vertically upwards. The gases are exhausted vertically downwards with velocity \(100 \mathrm{~ms}^{-1}\) with respect to the rocket. What is the minimum rate of burning of fuel, so as to just lift the rocket upwards of fuel, so as to just lift the rocket upwards against, the gravitational attraction? (Take \(g=10 \mathrm{~ms}^{-2}\) )