372208 A satellite in a force free space sweeps stationary interplanetary dust at a rate. \(\left(\frac{\mathbf{d M}}{\mathbf{d t}}\right)=\alpha \mathrm{v}\). The acceleration of satellite is

372209 Physical independence of force is a consequence of

372210 The force on a rocket moving with a velocity \(300 \mathrm{~m} / \mathrm{s}\) is \(210 \mathrm{~N}\). The rate of consumption of fuel of rocket is

372211 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 \(\left(\mathrm{g}=10 \mathrm{~ms}^{-2}\right)\)

372208 A satellite in a force free space sweeps stationary interplanetary dust at a rate. \(\left(\frac{\mathbf{d M}}{\mathbf{d t}}\right)=\alpha \mathrm{v}\). The acceleration of satellite is

372209 Physical independence of force is a consequence of

372210 The force on a rocket moving with a velocity \(300 \mathrm{~m} / \mathrm{s}\) is \(210 \mathrm{~N}\). The rate of consumption of fuel of rocket is

372211 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 \(\left(\mathrm{g}=10 \mathrm{~ms}^{-2}\right)\)

372208 A satellite in a force free space sweeps stationary interplanetary dust at a rate. \(\left(\frac{\mathbf{d M}}{\mathbf{d t}}\right)=\alpha \mathrm{v}\). The acceleration of satellite is

372209 Physical independence of force is a consequence of

372210 The force on a rocket moving with a velocity \(300 \mathrm{~m} / \mathrm{s}\) is \(210 \mathrm{~N}\). The rate of consumption of fuel of rocket is

372211 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 \(\left(\mathrm{g}=10 \mathrm{~ms}^{-2}\right)\)

372208 A satellite in a force free space sweeps stationary interplanetary dust at a rate. \(\left(\frac{\mathbf{d M}}{\mathbf{d t}}\right)=\alpha \mathrm{v}\). The acceleration of satellite is

372209 Physical independence of force is a consequence of

372210 The force on a rocket moving with a velocity \(300 \mathrm{~m} / \mathrm{s}\) is \(210 \mathrm{~N}\). The rate of consumption of fuel of rocket is

372211 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 \(\left(\mathrm{g}=10 \mathrm{~ms}^{-2}\right)\)