Hello guys,
I am stuck on a physics question. Although I know the procedure to solve it but I am not good at calculating numbers. I mess up a lot when I am calculating.
Calculate how much fuel was used when ISS ( international space station) corrects its orbits. The fuel flows at 0.32(kg/s) through the progress engines when the process starts. The re- boost of orbit applies a Delta V of precisely 24.6942 (m/s). The space station's mass is 246733kg. The combined thrust of engines is 821.3 Newtons of force. Answer must be in (kgs)
Procedure of what I did:
First calculate acceleration using F= M•A - which is dividing the 821.3N/ 246733 kg = getting answer in m/s squared
Then dividing the Delta V to the Acceleration that we found above to get the engine burn time.
Then divide it by the fuel flow rate of 0.32 (kg/s) to get how much fuel will be used.
I am stuck on a physics question. Although I know the procedure to solve it but I am not good at calculating numbers. I mess up a lot when I am calculating.
Calculate how much fuel was used when ISS ( international space station) corrects its orbits. The fuel flows at 0.32(kg/s) through the progress engines when the process starts. The re- boost of orbit applies a Delta V of precisely 24.6942 (m/s). The space station's mass is 246733kg. The combined thrust of engines is 821.3 Newtons of force. Answer must be in (kgs)
Procedure of what I did:
First calculate acceleration using F= M•A - which is dividing the 821.3N/ 246733 kg = getting answer in m/s squared
Then dividing the Delta V to the Acceleration that we found above to get the engine burn time.
Then divide it by the fuel flow rate of 0.32 (kg/s) to get how much fuel will be used.