Question

A Space ship of mass 5000 kg is heading towards the moon and wants to change...

A Space ship of mass 5000 kg is heading towards the moon and wants to change its trajectory by 20 degrees relative to original path. The rocket has a velocity of 110 m/s. How much gas must be used up if it burns its rockets (using up fuel) and expels gas at a velocity of 1200 m/s (perpendicular to its direction of motion)?

Homework Answers

Answer #1

given,

mass of the rocket = 5000 kg

velocity = 110 m/s ,angle = 20 degree

gases are expelled at speed = 1200 m/s

sideways velocity / radial velocity = tan(20)

Therefore the rocket will have a sideways momentum of

(M-m) * sideways velocity = (M-m) * radial velocity * tan(20)

where, M = initial rocket mass

m = mass of the gas expelled This sideways momentum will be balanced by the momentum of the gases expelled

m *1200 = (5000kg - m) *110* tan(20)

m*1200=200183.62 - 40.36*m

1240.36*m=200183.62

This gives

m = 161.43 kg

mass must be expelled = 161.43 kg

Know the answer?
Your Answer:

Post as a guest

Your Name:

What's your source?

Earn Coins

Coins can be redeemed for fabulous gifts.

Not the answer you're looking for?
Ask your own homework help question
Similar Questions
A space probe (mass = 4.85 x 102 kg) is drifting directly toward the moon (in...
A space probe (mass = 4.85 x 102 kg) is drifting directly toward the moon (in the +x direction) at a speed of 3.23 x 104 m/s. To correct its speed before going into orbit, a thruster rocket is fired in the -x direction; the magnitude of the force is 5.63 x 104 N. The speed after the thruster is fired is 2.87 x 104 m/s. a. Find the probe’s momentum before the thruster is fired, as well as its...
Ion-propulsion rockets have been proposed for use in space. They employ atomic ionization techniques and nuclear...
Ion-propulsion rockets have been proposed for use in space. They employ atomic ionization techniques and nuclear energy sources to produce extremely high exhaust velocities, perhaps as great as 8.00×10^6m/s. These techniques allow a much more favorable payload-to-fuel ratio. To illustrate this fact: (a) Calculate the increase in velocity of a 20,000-kg space probe that expels only 40.0-kg of its mass at the given exhaust velocity. (b) These engines are usually designed to produce a very small thrust for a very...
A jet accelerates at a=3.92 m/s^2 from rest until it reaches its takeoff velocity of 360...
A jet accelerates at a=3.92 m/s^2 from rest until it reaches its takeoff velocity of 360 km/hr. It has to travel for 5 seconds at its takeoff velocity before taking off. What's the minimum distance that the jet will travel on the runway? A car backs up at a constant speed for a short time, then applies the brakes and steadily comes to rest. Sketch velocity-time and position-time graphs that depict the car's motion. Assume that the forward direction is...
The mass of the Sun M = 2.0×1030 kg, and G = 6.67×10-11 Nm2 /kg2 a)....
The mass of the Sun M = 2.0×1030 kg, and G = 6.67×10-11 Nm2 /kg2 a). A spaceship of mass m = 7.5×104 kg is on a circular orbit of radius r1 = 2.5×1011 m around the Sun. The captain of that spaceship decides to increase the radius of his orbit to r2 = 4.0×1011 m. What is the minimum amount of energy he has to expand using his engines to move to this higher orbit? [Assume that the ship...
21) A person carries a 25.0-N rock through the path shown in the figure, starting at...
21) A person carries a 25.0-N rock through the path shown in the figure, starting at point A and ending at point B. The total time from A to B is 1.50 min. How much work did gravity do on the rock between A and B? A) 625 J B) 20.0 J C) 275 J D) 75 J E) 0 J 22) A person carries a 2.00-N pebble through the path shown in the figure, starting at point A and...
ADVERTISEMENT
Need Online Homework Help?

Get Answers For Free
Most questions answered within 1 hours.

Ask a Question
ADVERTISEMENT