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
A rocket of mass 1.5 x 10^6 kg is launched upward from the surface of the Earth (mass ME = 5.97 x 10^24 kg, radius RE = 6.38 x 10^6 m) with a speed of 0.5 x 10^4 m/s. The rocket will reach a maximum altitude above the surface of the Earth of
Homework Equations
I...
I have no idea if I am picturing this whole scenario wrong, so please hear me out and try to point me in the right direction.
Anyways, say we have a fast moving rocket with a person in it. Lightning strikes a side of it. So the light traveling from the bolt to the person/observer is traveling...
Homework Statement
A rocket ejects pressurized air with constant relative velocity v_{rel} and moves horizontally. Starting from rest and an initial mass m_{1}, find the speed of the rocket when its mass is m_{2}(m_{2}<m_{1}). How does this result depend on the rate r=dm/dt at which the air...
One of the biggest problems with launching things into space is that fuel weighs a lot. With conventional rocketry, mass of fuel per unit of stored energy is high enough that it requires huge rockets to lift even a couple of tons into orbit.
Electrons are very light, and can be used to store...
Homework Statement
You must determine the acceleration of a rocket so that its equipment can be deisgned to survive. The rocket will have a burn time of t = 30secs, during which time it flies straight up with a constant acceleration a; call this "Phase 1" of the experiment. After the fuel is...
Still preparing for a classical prelim. Not sure if my solution is correct. Any help is more than appreciated.
Homework Statement
According to specifications, the five Saturn V booster engines collectively supplied a liftoff thrust of 34 \times10^{6}N. The specific impulse was 2580...
Homework Statement
I have to design a two-stage rocket to accelerate a payload of 100kg from rest to a final velocity of 6,000 m/s (no gravity to worry about) using the minimum amount of mass for the rocket stages.
Each stage of the rocket must obey the following restriction:
Whatever...
Let’s consider Galileo’s description of relativity of motion using the example of a moving ship. The ship is at rest and made to accelerate extremely slowly for a few minutes, and then moves at a constant velocity. When the ship is moving at some constant velocity, the contents of the ship will...
Suppose a rocket is hovering above the moon at a constant height, burning just enough propellant to stay at that height, and not move upwards or downwards.
Viewed from an inertial frame, we have. Initial energy (just before ignition) :
1. Gravitational potential energy between rocket and...
I've been thinking. Would it be any more efficient to use the angular momentum of a spinning rocket engine nozzle to eject the rocket fuel? Just an idea. Post any questions below
Homework Statement
So you're shooting off a water rocket, which has some water inside a 2L soda pop bottle. You're then pumping (for example, a bicycle pump) to compress more and more air inside to a higher pressure.
Homework Equations
Well, work = F*d. If you measure the stroke of the...
Homework Statement
A model rocket is launched straight upward with an initial speed of 50.0 m/s. It accelerates with a constant upward acceleration of 2.00 m/s^2 until its engines stop at an altitude of 150 m. How long after lift off does the rocket reach the maximum height?
from...
I'm currently working on a bottle rocket for my physics class. Instead of taking the assigned experiment, a friend and I have chosen a side experiment to work on.
The experiment: Create a rocket using a 2L bottle as a compression chamber and compare the time required to reach the apex of its...
Hello Everyone,
If I were to blast off my model rocket from a weather balloon what altitude would it reach?
I have a model rocket that routinely reaches 10,000' @ sea level. If this were attached to a weather balloon and launched at 100,000', what would happen? Are gravitational pull...
I started taking MIT's online physics course a couple of days ago, and since I have no physics background at all, I'm getting a bit confused with dimensional analysis.
I'm trying to find a formula for the terminal velocity of a rocket, using air density ρ, gravity g, area of rocket affected by...
Bottle Rocket Fuels (URGENT)
Assuming the same volume, which should travel higher - a bottle filled with a dense fluid or a bottle filled with a less dense fluid?
Thanks for reading!
Suppose I am building a rocket for interstellar travel. I want it to be able to go as fast as possible for a given fuel load.
Since the momentum of my rocket will equal the momentum of the fuel I eject from the back of it, it behooves me to eject the fuel with as high a velocity as possible...
Hi everyone,
My high school class is doing a competition where we have to build a rocket out of a 2L pop bottle powered by compressed CO2 and launch it (not directly up but at an angle)
we need to...
-achieve maximum distance
-have minimimal horizontal deviation
-protect an egg that the...
I am building a water rocket for my physics class and I want to make my calculations as precise as possible. I want to calculate throttle, velocity, acceleration, momentum, and max height.
With that said, what should I take into account? Gravity, wind velocity, shape of cone of the rocket...
Homework Statement
So we launched small rockets on our last day, but have a week to turn in the homework based on the launch, but seeing as we aren't allowed back in school I can't ask questions I am lost. We haven't dealt with anything remotely related to trajectory since the beginning of...
Homework Statement
A rocket of (time dependant) mass M ejects fuel such that its change in mass in the instantaneous ZMF is \frac{dM}{d\tau} = -\frac{E}{c^2} The speed of the fuel ejected is w.
Prove that a = \frac{Ew}{Mc^2}
where a is defined by -a^2 = A_\mu A^\mu
The Attempt at...
A livestream video feed from the event has started and can be accessed via the CS homepage [1] or the corresponding blog on Wired [2]. Some background information about CS can be found on [3] together with a (very) short description on the TM65 [4].
[1] http://www.copenhagensuborbitals.com/
[2]...
When I was at Uni, in the 60s, we had a brief course on 'Space Physics'. It had a hotch potch of topics in it and one of them was about actually launching satellites.
'In those days', apparently, vehicles were rotated during the launch and this rotation had to be eliminated once they were in...
Hey,
I have a question on a rocket in deep space (all external forces negligible), basically I'm doing something wrong the latter part of the question - maximizing the momentum via differentiation, here's the question:
So the momentum at a given mass 'm' is ...
Homework Statement
Rocket motors make a rocket of mass of 2200kg accelerate at 2.5m/s^2 over a distance of 650m in deep space. What is the work done?
The Attempt at a Solution
F=m*a 2200kg*2.5m/s^2 = 5500N
5500*650= 3575000
When I look at the answer page it tells me the force...
I worked through a simple twin paradox problem, and I think I have the correct solution. However, I wanted to confirm that my numbers are correct. There is nothing fancy about the solution, but it resolves the "paradox" completely for me. Every other resolution I have looked at either leaves...
Suppose we have a satellite in an elliptical orbit around the Earth with the major axis pointed towards some fixed point in the heavens. What is the minimum number of rocket burns so that the major axis is rotated 90 degrees and the final and initial energy are the same. Is the number 2?
At...
Because this is not a 'formal' question I won't use the template.
I was wondering, what if I have a rocket (varying mass) with air resistance acting upon it?
Let's say the F=-kv
u is the speed of the rocket relative to the gas, and the rate of mass/second extracted is
b
without g it would...
If a rocket is traveling past the Earth at speed v, and the time interval measured by the astronaut is four times smaller than the time interval measured by an observer on the Earth. What is the value of v
I have attempted the solution and got:
Δt=γΔt'
Where i believe that gamma will be...
Mythbusters did a test to see if a water heater would shoot through the roof of a two story building (home). They close all orfices, heated the water and it soared through the roof. They computed the final pressure as 85,000 pounds. As I recall they computed this by multiplying the area of the...
Homework Statement
A rocket passes the Earth at 0.8c. As it goes by, it launches a projectile at 0.6c perpendicular to the direction of motion. What is the projectile's speed in the Earth's reference frame?
Homework Equations
[;u=\frac{u'+v}{1+u'v/{c}^{2}};]
The Attempt at a Solution
Since...
So I have been thinking and there's probably a good reason why it doesn't exist already but i'll go ahead and share my idea here on the forums. How about making something similar to the hadron collider but the tube that runs underground is capable of housing the space shuttle. It sits on rail...
Alright everybody, I REALLY need help on this and I only have a limited time. So I took a video of a model rocket and using the video analysis software, Tracker, I have a graph of position vs. time. Now I don't know calculus yet (only in pre-calc as of now), so the derivation of the graph won't...
Hello Forum,
Let us review about rocket move.The Rocket moving with 2 mechanical principe;Newton's 3 and conservation of momentum.If rocket at t=0 is in rest condition (E=0),after the gas with dm mass go out to the back from rocket ,then rocket move to the front(E=Ek1+Ek2).
Nothing external...
I am doing an assignment about launching a rocket and at the moment I am looking for the delta V of the rocket. I have done a few researches and i found a method of finding the energy of the rocket and find the delta vee of it , but then i found this article and I am not sure if it is delta vee...
So, I need to make an Excel spreadsheet that realistically models the motion of a toy rocket. I need to take drag, gravity, and thrust into account, keeping in mind that the latter two will be influenced by the change in mass. The equation for force I must use, then, is:
F = ma + v(dm/dt)...
Homework Statement
A warlock testing a rocket broom takes off from a standing start and flies at fixed elevation. The warlock and fueled rocket system start out with mass Mi. The rocket fires with exhaust speed u, losing mass at a constant rate R, and we’ll assume air drag is negligible. If...
When a rocket is launched, it starts not with velocity zero, but with the rotation velocity which the Earth gives it. Thus if a rocket is launched eastward, it requires a smaller boost (and if westward, a larger one) to achieve orbit. with a latitude of 31.1 degrees, cos(31degrees) 24902/24 =...
Homework Statement
A 10.1 kg weather rocket generates a thrust of 193.0 N. The rocket, pointing upward, is clamped to the top of a vertical spring. The bottom of the spring, whose spring constant is 415.0 N/m, is anchored to the ground.
(a) Initially, before the engine is ignited, the rocket...
Homework Statement
Do rockets have linear or exponential acceleration?
The Attempt at a Solution
This is not a homework question I was just wondering if Rockets have linear or exponential acceleration. I was thinking that they have exponential acceleration because of the constant loss of mass...
Homework Statement
A rocket is launched vertically up with no initial velocity. Propulsion is provided by the ejection of mass with constant velocity of ejection u = 66.0 m/s relative to the rocket and at a constant rate so determined that the initial acceleration is zero. The mass of fuel...
Hi everyone,
Quick question I may just not be thinking right here but I was trying to find the acceleration, velocity, and position of a rocket as a function of time. I started with acceleration:
a =\frac{T}{m-\dot{m}t} - g where T is the Thrust, m is the initial mass, mdot is the mass flow...
Homework Statement
The pilot of a rocket wants to reach a star in 1 year. The rocket is currently on Earth. The star is 4 light years away, measured from an observer on Earth. What velocity is needed for the pilot to reach the star in a year in the pilot's/rocket's time?
Homework Equations...
Homework Statement
I a little lost on how to use the relativistic velocity addition formula to determine the increase in speed "v" over a short time interval in the Earths frame of reference, for a rocket having left Earth at rest and traveling through space accelerating at constant acc. of...
I know I've done this problem a few times before but I'm just a fumbling idiot at the moment..
Homework Statement
Rocket has an acceleration of 12m/s^2 and at an altitude of 1km the motor shuts off. What is the maximum height?
Homework Equations
V^2=V_i+2a(x_f-X_i)...
Homework Statement
Consider a rocket is subject to linear resistive force, f = -bv . \dot m is constant. Use the equation: m \dot{v} = -\dot{m }v + f to determine the velocity of the rocket :
since the rate of mass lost is constant
let \dot{m} =k
vex = nuzzle velocity
v = \frac{k}{b}...
Hi all,
Does anyone know where I can find the formula for the relavistic rocket equation? That is, I want to know the mass of fuel required to accelerate a rocket from 0 to β, for a given acceleration A, assuming the rocket (with no fuel) has a mass of M. All of this would be in the frame of...
Homework Statement
Find the speed v of the rocket when the mass of the rocket = m. The rocket starts from rest at with mass M. Fuel is ejected at speed u relative to the rocket.
Homework Equations
m1v1 = m2v2
The Attempt at a Solution
In the textbook, it starts off with a moving...
I'm modelling a rocket leaving to outer space and I want to incorporate air resistance in the model. I however have no clue what the drag coefficient as well as the cross sectional area of a typical rocket would be. Can someone help me on this?