Determine the mass ratio (Burnout mass/ Initial mass) of a vehicle in a gravitation less space if its velocity is boosted from 800 m/s to 1600 m/s and the effective rocket exhaust velocity is 2000 m/s.

Flight Performance topics include: Gravity free drag free space flight performance, vehicle forces in the atmosphere, motion basic relations, vehicles propulsion system effect, space flight, exhaust plumes aerodynamic effect, flight stability, flight performance on military missiles, flight maneuver and vehicles. The fundamental measure of rocket engine performance is the mass of propellant that can be propelled out the back of the rocket and at what speeds. The performance of a rocket engine depends on the thrust, which is generated relative to the size or weight of the propulsive... Show more

Flight Performance topics include: Gravity free drag free space flight performance, vehicle forces in the atmosphere, motion basic relations, vehicles propulsion system effect, space flight, exhaust plumes aerodynamic effect, flight stability, flight performance on military missiles, flight maneuver and vehicles.

The fundamental measure of rocket engine performance is the mass of propellant that can be propelled out the back of the rocket and at what speeds. The performance of a rocket engine depends on the thrust, which is generated relative to the size or weight of the propulsive device. 

The most important metric for the efficiency of a rocket engine is specific impulse, which is measured as a speed or a time. The higher the specific impulse, the less propellant is required to provide the desired impulse. 

The performance of a rocket is determined by the propellant flow rate (Mo) in kilograms/second and the effective exhaust velocity (Ve) in meters/second. 

Show less