3. A rocket of mass 10,000 kg will have an escape velocity __________ the escape
velocity of a rocket with mass 5,000 kg.
A. one quarter of
B. one half of
C. the same as
D. double
here,
for the escape velocity
the escape velocity = sqrt(2 * G * M/R)
the escape velocity is independent of the mass of the rocket
therefore,
the escape velocity C. the same as the escape velocity of a rocket with mass 5000 Kg
3. A rocket of mass 10,000 kg will have an escape velocity __________ the escape velocity...
Gravitational Fields: a) What is the escape velocity for a stationary object (of mass 100 kg) from a planet if an object dropped on its surface falls 5m in 1.4 seconds. (diameter of planet is 12,000 km) b) What is the objects velocity at a distance of 60, 000 km if the velocity is 1.2 times the escape velocity? Please show and explain as much work as possible. Thank you!
Gravitational Fields: a) What is the escape velocity for a stationary object (of mass 100 kg) from a planet if an object dropped on its surface falls 5m in 1.4 seconds. (diameter of planet is 12,000 km) b) What is the objects velocity at a distance of 60, 000 km if the velocity is 1.2 times the escape velocity? Please show and explain as much work as possible. Thank you!
The escape velocity is a function of a planet’s radius and mass. We also know that the mass of an object is M = ρV where ρ is the mass density and V is the volume. The volume of a sphere is V = (4/3) π R3 a.) combine the formula for the escape velocity with the additional relationships given above and find an expression for the escape velocity as a function of the mass density and radius of a...
The escape velocity for the planet with a mass of 8.00 x 10^25 kg and a radius of 24,500 km is ____ m/s.
Rockets! Find the minimun fuel exhaust rate of the launch escape system, a secondary small rocket used to save crews in case of rocket failure, if the main rocket's exhaust velocity is 10m/s and fuel exhaust rate is 3000kg/s. The mass of the escape system is 3 tons , and the its exhaust velocity is 5 km/s.The mass of the entire system is 500 tons.
If the escape velocity of the Earth is approximately 12 km/s. What is the escape velocity for a planet whose radius is 4 times, and whose mass is 100 times that of Earth? a. 1.2 km/s b. 12 km/s c. 60 km/s d. 300 km/s e. 600 km/s
A fully fueled rocket has a mass of 21000 kg, of which 25000 kg is fuel. The burned fuel is exhausted at a rate of 190 kg/s at a speed of 2800 m/s relative to the rocket. If the rocket is fired vertically upward, calculate.... a.) The trust of the rocket b.) The net force on the rocket at blastoff and just before burnout (when all the fuel has been used up) c.) The rocket's velocity at burnout *** Ignore...
I'd question 40 please.
39. Rocket Motion Suppose a small single-stage rocket of total mass m) is launched vertically, the positive direction is upward, the air resistance is linear, and the rocket consumes its fuel at a constant rate. In Problem 22 of Exercises 1.3 you were asked to use Newton's second law of motion in the form given in (17) of that exercise set to show that a mathematical model for the velocity v(t) of the rocket is given...
1. For an ideal rocket with a characteristic velocity of c 1220 m/s, a mass flow rate of 73 kg/s, a thrust coefficient of 1.5 and a nozzle throat area (A0.0248 m2), compute a. The effective exhaust velocity, c b. The thrust, F c. The chamber pressure, pc d. And the specific impulse, Isp
A rocket with a mass of 1000 kg is placed vertically on the launch pad. If the rate the propellants are consumed is 2 kg/s, determine the exhaust velocity required when the rocket just begins to rise.