Lag1989 task 3.23
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The initial mass of the rocket is m₀ = 200 g, the mass of the charge is m = 180 g, the initial velocity of the rocket is zero, the relative exit velocity of the combustion products of the nozzle is u = 30 m / s. Neglecting air resistance and the acceleration of free fall, find the speed of the rocket at the time of full charge burnout.
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- Content type File
- Content description 32,84 kB
- Added to the site 10.08.2022
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Lag1989 task 3.23
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Timur_ed
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| 15 $ | the discount is 20% |
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Timur_ed
1
Cumulative discount
| 15 $ | the discount is 20% |
Check your discount
Amount of purchases from the seller: $
Your discount: %