Diwali rocket is ejecting 50 g of gases/s at a velocity of 400 ms-1. The accelerating force on the rocketwill be [RPMT 2011]
22 dyne
20 N
20 dyne
100 N
The accelerating force on the rocket = upward thrust
=ΔmΔt·v
Given, ΔmΔt=50×10-3kgs-1
and v=400 ms-1
So, accelerating force =50×10-3×400=20 N