Home
Class 11
PHYSICS
A 500kg rocket is set for verticle firin...

A 500kg rocket is set for verticle firing. The exhaust speed is 800`ms^-2` . To give an initial upward acceleration of 20`ms^-2` , the amount of gas ejected per second to supply the needed thrust will be (g=10 `ms^-2` )

A

`127.5 kg s^(-1)`

B

`137.5 kg s^(-1)`

C

`187.5 kg s^(-1)`

D

`185.5 kg s^(-1)`

Text Solution

Verified by Experts

The correct Answer is:
C

`F=(dp)/(dt), m(g+a)=(dm)/(dt)v rArr (dm)/(dt)=(m(g+a))/(v)`
Promotional Banner

Topper's Solved these Questions

  • LAW OF MOTION

    NARAYNA|Exercise EXERCISE - I (C.W)(IMPULSE)|6 Videos
  • LAW OF MOTION

    NARAYNA|Exercise EXERCISE - I (C.W)(OBJECTS SUSTENDED BY STRINGS & APPARENT WEIGHT)|9 Videos
  • LAW OF MOTION

    NARAYNA|Exercise C.U.Q|73 Videos
  • KINETIC THEORY OF GASES

    NARAYNA|Exercise LEVEL-III(C.W)|52 Videos
  • MATHEMATICAL REVIEW & PHYSICAL WORLD

    NARAYNA|Exercise C.U.Q|13 Videos

Similar Questions

Explore conceptually related problems

A 500kg rocket is set for verticle firing. The exhaust speed is 800ms(-2) . To give an initial upward acceleration of 20ms(-2) , the amount of gas ejected per second to supply the needed thrust will be (g=10ms(-2)

A 5000 kg rocket is set of vertical firing. The exhaust speed is 800" "ms^(-1) . To give an initial upward acceleration of 20ms^(-2) , the amount of gas ejected per second to supply the needed thrust will be (take, g=10ms^(-2) )

A 5000 kg rocket is set for vertical firing. The exhaust speed is 800 m//s . To give an initial upward acceleration of 20 m//s^(2) , the amount of gas ejected per second to supply the needed thrust will be (Take g = 10 m//s^(2) )

A 500 kg rocket is set of vertical firing. The relative speed of burnt gas is 800ms^(-1) To give an initial upwards acceleration of 20ms^(-2) , the amount of gas ejected per second to supply the needed thrust will be

A 1000kg rocket is set for vertical firing. The exhaust speed is 500m//s .To give the rocket an initial upward acceleration of 30 m//s^(2) , the amount of gas ejected per second to supply the needed thrust is

A 5000 kg rocket is set for verticle firing the relative speed of burnt gas is 800ms^(-1) To give an initial upwards acceleration of 20ms^(-2) the amount of gas ejected per second to supply the needed thrust will be

A 2000 kg rocket is set for vertical firing the exhaust speed is 400 m/s to given an initial upward acceleration of 10m//s^(2) . Find out the amount of gas ejected per second to supply the needed thrust (g=10m//s^(2))