EyezsoLow
10+ year member
Senior VIP Member
Prove that the upward velocity of a rocket of initial mass M0, which is propelled by fuel burning at a rate of R kg/s, is given by vy = uex * ln[M0 / M(t) ] - g * t. uex is the speed of the exhaust gas relative to the rocket and M0 is the initial mass (rocket + fuel).
Also find the initial velocity and acceleration and velocity at time = 180s.
M0 = 2.12E6 kg
Fth = 2.32E7 N (Force of thrust)
R = 4.6E3
M(t) = M0 - R * t
Fth = -R * uex
No idea what to do or where to start...
Also find the initial velocity and acceleration and velocity at time = 180s.
M0 = 2.12E6 kg
Fth = 2.32E7 N (Force of thrust)
R = 4.6E3
M(t) = M0 - R * t
Fth = -R * uex
No idea what to do or where to start...
