A rocket (from Italian: rocchetto, lit. 'bobbin/spool') is a projectile that spacecraft, aircraft or other vehicles use to obtain thrust from a rocket engine. Rocket engine exhaust is formed entirely from propellant carried within the rocket. Rocket engines work by action and reaction and push rockets forward simply by expelling their exhaust in the opposite direction at high speed, and can therefore work in the vacuum of space.
In fact, rockets work more efficiently in space than in an atmosphere. Multistage rockets are capable of attaining escape velocity from Earth and therefore can achieve unlimited maximum altitude. Compared with airbreathing engines, rockets are lightweight and powerful and capable of generating large accelerations. To control their flight, rockets rely on momentum, airfoils, auxiliary reaction engines, gimballed thrust, momentum wheels, deflection of the exhaust stream, propellant flow, spin, or gravity.
Rockets for military and recreational uses date back to at least 13th-century China. Significant scientific, interplanetary and industrial use did not occur until the 20th century, when rocketry was the enabling technology for the Space Age, including setting foot on the Earth's moon. Rockets are now used for fireworks, weaponry, ejection seats, launch vehicles for artificial satellites, human spaceflight, and space exploration.
Chemical rockets are the most common type of high power rocket, typically creating a high speed exhaust by the combustion of fuel with an oxidizer. The stored propellant can be a simple pressurized gas or a single liquid fuel that disassociates in the presence of a catalyst (monopropellant), two liquids that spontaneously react on contact (hypergolic propellants), two liquids that must be ignited to react (like kerosene (RP1) and liquid oxygen, used in most liquid-propellant rockets), a solid combination of fuel with oxidizer (solid fuel), or solid fuel with liquid or gaseous oxidizer (hybrid propellant system). Chemical rockets store a large amount of energy in an easily released form, and can be very dangerous. However, careful design, testing, construction and use minimizes risks.
Homework Statement
I need to find the final velocity of a multistage rocket (accelerating from rest in free space) that burns its fuel in two stages. In the first stage, it burns 3/10 of its initial mass as fuel. Then it jettisons its first-stage fuel tank, which has a mass of 1/10 the...
Homework Statement
Calculate the force exerted on a rocket, given that the propelling gases are expelled at a rate of 1000 kg/s with a speed of 60,000 m/s (at takeoff)
Homework Equations
p=mv
F\Delta{t} = \Delta{p}
The Attempt at a Solution
This is probably the first question I am...
Homework Statement
Obviously, we can make rockets to go very fast, but what is a reasonable top speed? Assume that a rocket is fired from rest at a space station in deep space, where gravity is negligible.
If the rocket ejects gas at a relative speed of 1100 and you want the rocket's...
Homework Statement
A rocket is fired straight up from the surface of the Earth at half the escape velocity. How high will it go relative to the surface of the earth?
Neglect dissipative forces.
Homework Equations
Uinitial + Kinitial = Uf
Kf is zero
G*m*M/radius^2 + 1/2mv^2 =...
The Basis of this question is that:
* Rockets launched at an angle follow the path of a rectangular hyperbola when thrust greater than their mass is produced.
* That rockets fall in the path of a parabola when thrust is no longer produced, this only applies when the rocket has both x and y...
A model rocket is launched with an upward acceleration, after t seconds it runs out of fuel at x height. Sketch the a vs. t, v vs. t, and position vs. t graphs for the rocket from the time of launch until the moment it reaches max height.
-I know that after the rocket runs out of fuel it will...
About stabilizing a space rocket using a pendullum
There exists a competition called Google Lunar X Prize whose main objective is sending a rocket to the Moon. One of the contenders, team ARCA, is ready to launch a rocket (not a Moon rocket) about which they claim to be passively stabilized...
This is my first posting - I don't know whether its on the right section but I have a question
is there a formula to work out
how much thrust you need to get a certain weight of rocket up in the air, also for the rockets altitude?
Thanks
Homework Statement
A rocket car is developed to break the land speed record along a salt flat in Utah. However, the safety of the driver must be considered, so the acceleration of the car must not exceed 5g (or five times the acceleration of gravity) during the test. Using the latest materials...
I don't know if I posted on the right forum but I know I'm on the right site.
I'm planning to create my first homemade rocket that can fly maybe hundreds of feet or less then it will parachute down after peacefully.
I'm not an engineer but if you willing to help me, I would feel how to...
Could you please help me find experimental error in bottle rocket experiment that could have affected my results. The experiment is where a bottle gets filled with water, a third of their volume and then they get pressurized to fly in the air.
So could you please find me experimental errors...
Homework Statement
A model rocket blasts off from the ground, rising straight upward with a constant acceleration that has a magnitude of 76.0 m/s2 for 1.54 seconds, at which point its fuel abruptly runs out. Air resistance has no effect on its flight. What maximum altitude (above the ground)...
Homework Statement
A two stage rocket is launched with an average acceleration of +4 m/s/s. After 10 seconds, a second stage is activated and the rocket's acceration is now +6 m/s/s.
Part A: Find the vertical displacement of stage one of the rocket, before accleration changes to 6...
Homework Statement
A two stage rocket is launched with an average acceleration of +4 m/s/s. After 10 seconds, a second stage is activated and the rocket's acceration is now +6 m/s/s.
Part A: Find the vertical displacement of stage one of the rocket, before accleration changes to 6...
Homework Statement
To illustrate the use of a multistage rocket consider the following:
(a) A certain rocket carries 60% of its initial mass as fuel. (That is, the mass of fuel is .6m0). What is the rocket's final speed, accelerating from rest in free space, if it burns all its fuel in...
Homework Statement
A rocket (initial mass m0) needs to use its engines ot hover stationary, just above the ground. If it can afford to burn no more than a mass (lamda)m0 of its fuel, for how long can it hover? If the exhaust velocity is 3000 m/s and lambda is 10% how long can the rocket...
Homework Statement
A rocket is fired at a speed of 75.0 m/s from ground level, at an angle of 60.5° above the horizontal. The rocket is fired toward an 11.0 m high wall, which is located 22.5 m away. The rocket attains its launch speed in a negligibly short period of time, after which its...
One idea that just came to me relates to the "pendulum fallacy", whereby people mistakenly think that a rocket is hanging by the nose from an imaginary string, instead of actually resting on top of its tail/thruster.
So then, what if you could position a lot more of the rocket/lander's mass...
A rocket is fired vertically upwards with an initial velocity of 80 m/s with an acceleration of 4 m/ss until it reaches an altitude of 1000m. At that point it goes into free fall (a= -9.8)
What time interval is the rocket in the air?
What is its maximum altitude?
What is its velocity...
Kinematics Model Rocket problem !
A) A model rocket is launched straight upward with an initial speed of 49.6 m/s. It accelerates with a constant upward acceleration of 1.83 m/s2 until its engines stop at an altitude of 155 m. What is the maximum height reached by the rocket?
B) How long...
Homework Statement
A rocket is launched at an angle of 53 degrees above the horizontal with an initial speed of 100 m/s. The rocket moves for 3.00s along its initial line of motion with an acceleration of 30.0 meters per second squared. At this time, its egines fail and the rocket proceeds to...
Homework Statement
A rocket, initially at rest on the ground, accelerates straight upward from rest with constant net acceleration a, until time t1, when the fuel is exhausted.
Find the maximum height H that the rocket reaches (neglecting air resistance).
Express the maximum height in...
can someone please help me??
I thought I had the answer to this problem, but it doesn't match the book's answer. I can't figure out what I'm doing wrong. This is the problem:
A rocket is launched straight up with constant acceleration. 4 seconds after liftoff, a bolt falls off the rocket and...
Homework Statement
A model rocket has been fired with V0=50m/s at 35 degrees above horizontal. Find magnitude and direction at t=4s.
Homework Equations
V = V0+at, displacement = v0t + .5at2
The Attempt at a Solution
I have successfully found the magnitude by setting Vx= 50*cos35...
Homework Statement
A rocket with that has a proper length of 1100 m moves away from a space station in the + x direction at 0.60c relative to an observer on the station. An astronaut stands at the rear of the rocket and fires a dart toward the front of the rocket at 0.85c relative to the...
We need to design a model rocket from scratch that is resistant to crosswinds and keep its trajectory withing a target zone.
Does anyone know any methods to keep a model rocket stable in windy conditions?
My idea was to make the rocket rather heavy, to resist the force of the wind. Would...
State the fundamental equation of motion for a particle of variable mass.
A rocket of initial mass m0 is fired vertically, under the influence of a uniform gravitational field, and expels propellant at a constant relative velocity c downwards. The propellant is completely consumed after a...
So, the rocket equation is
F_ext = m(dv/dt) + u(dm/dt)
where m is the mass of the rocket, v the velocity, u the effective exhaust gases speed, and F_ext the external forces on the system.
If we take a constant mass ejection rate p, and take the external force to be the gravitational...
A model rocket with a mass of 0.50 kg is fired vertically from the ground. Assume that it is streamlined enough that air resistance can be ignored. Suppose it ascends under the influence of a constant net force of 2.0 N acting in a vertical direction and travels for 6.0 s before its fuel is...
If I have a rocket constantly accelerating at some rate a, (requiring some constant force F), I want to know how much work is done by the rocket to travel a given proper length.
For example, a rocket traveling to alpha centauri at 1g acceleration half way and 1g acceleration the other half...
"Acceleration increased during S-IC flight for two reasons: decreasing propellant mass; and increasing thrust as F-1 engine efficiency improved in the thinner air at altitude."
This is from Wikipedia, so who knows. Why would a thiner atmosphere increase the thrust efficency of the engine...
First off, let me say that what I am working on has taken me a few days to get to work and I just can't figure it out. It is really frustrating so any help is really appreciated.
I have three igniters. They are connected to a circuit. Once a switch is turned to "on" the three igniters are...
I have questions:
1) twin 1 goes on a rocket flys to pluto at .99c and comes back to Earth (all uniform motion, somehow). When he gets back he sees twin 2 is older. But since twin 2 was moving away from him at .99c why doesn't twin 2 see him as older?
2) Why does something gain mass as it...
A rocket is moving upwards at 28.72 meters per second. Then, its engines are turned off. How much time will it take for it to come to a stop if it is traveling upwards exactly straight? Also, how far would the rocket have had traveled after its engines were shut off? The weight of the rocket is...
What is the Air/Propane mixture Ratio?
The Fuel Air Ratio of a Jet Engine is 15 to 1. This is for JP4.
What is the Fuel Air Ratio for Propane Gas?
I have learned the only difference between a rocket engine and pulse jet engine is the pulse jet runs on the oxygen that is in the air (30%...
I thought this was pretty cool. A private company (Space Exploration Technologies) has started launching rockets for customers.
Full story:
http://news.yahoo.com/s/nm/20090714/sc_nm/us_space_business_2
If a rocket is traveling upwards at 40.24 meters per second, how long will it take until gravity (9.81 m/s) causes the rocket to stop and go downards?
Also, if a rocket is traveling at 33.96 meters per second, and then its fuel runs out, and another rocket ignites immidiately after that at a...
I am trying to launch a rocket 200 feet away from the rocket. When the switch is thrown to "ON" the electrical circuit is turned on which sends an electrical current into the motors. I can launch the rocket just fine if I am standing right there to flip the switch, but as i increase the distance...
It is my understanding that when neon goes from a liquid to a gas, it has an expansion ratio of 1:1400. Would using N- and N+ be a realistic rocket fuel? I understand that it would take a lot of energy but is there a way to figure out how much?
One of the thought experiments Einstein proposed involved one twin staying on earth, while the second twin entered a shuttle. The twin in the shuttle went on a trip (a physical one), traveling near the speed of light. The twin in the shuttle would have time pass by slower than the one on the...
Homework Statement
A rocket is launched to travel vertically upward with a constant velocity of say...20 m/s.After
travelling maybe 35 s the rocket develops snag and its fuel supply is cut off. the rocket then travels like a free body, the height achieved by the rocket will be...
Homework Statement
I need to find the initial velocity of a rocket using the method a=\Deltav/\Deltat. Given a situation where \Deltat = 4 seconds. The force of gravity in this case is -10(m/s)
Homework Equations
After I get \Deltav how do I turn that into the initial velocity?
The...
A rocket is launched to travel vertically upward with a constant velocity of say...20 m/s.After
travelling maybe 35 s the rocket develops snag and its fuel supply is cut off. the rocket then travels like a free body, the height achieved by the rocket will be
THIS IS NOT A HOMEWORK QUESTION...
1)
How fast must a rocket travel on a journey to and from a distant star so that the astronauts age 12.0 years while the Mission Control workers on Earth age 130 years ? c
2)
As measured by Mission Control, how far away is the distant star? in light years
my attempt
1)
Time in...
Homework Statement
A 1222 kg weather rocket accelerates upward at 8.7 m/s2. It explodes 2.16 s after liftoff and breaks into two fragments, one twice as massive as the other. Photos reveal that the lighter fragment traveled straight up and reached a maximum height of 612 m. What was the...
Homework Statement
Find the gain in kinetic energy when a rocket emits a small amount of matter. (Well, there's more, but the rest of the question is built around this initial problem)...
The Attempt at a Solution
My logic revolves around the total kinetic energy of the rocket after...
Hi
Can anyone help to write rocket equation with strap on booster.
The exhaust velocity of the booster rocket and the core rocket is same? and
The exhaust velocity of the booster rocket and the core rocket is different?
Lost please help!
A 1974 kg weather rocket is launched straight up. The rocket motor provides a constant acceleration for 20.27 s, then the motor stops. The rocket altitude 23.94 s after launch is 7242. You can ignore any effects of air resistance.
What was the rocket's acceleration during...
Homework Statement
You are working on a project with NASA to launch a rocket to Mars, with the rocket blasting off from Earth when Earth and Mars are just aligned along a straight line from the sun. As a first step in doing the calculation, assume circular orbits for both planets. If Mars is...