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.
Hello
You have all been very helpfull with all my quistions about multi stage rockets and so, but I am only left with one quistion. I know a multi stage rocket is better, but can somebody show me a specific exambel where a single stage rocket is more advantageable, or link to a website where i...
Homework Statement
Hello all, I have to determine the maximum height of a model rocket.
The rocket is launched at an 45 degree angle
The finale velocity is 15,69 m/s (v)
the extutevelocety is 14,23 m/s (c)
The total mass is 180 gram (m) or m0)
The emty mass is 52 grams (mf)
The mass pr sek is...
Homework Statement
If the total relativistic velocity of small rocket is 0.75c after being launched from a larger rocket traveling at 0.60c, what is the velocity of the smaller rocket as observed from inside it?
Can someone put this in layman's for me please. I solved many relativistic...
Hey guys,
We all know that weight plays an important role in determining the speed of a vehicle, such as dragster like Top Fuel. But how about a rocket-powered dragster that uses hydrogen peroxide? Rocket-powered vehicles indeed accelerate faster than any wheel driven vehicle, but do weight...
how do i calculate the gradual reduction of angular momentum a rocket initially has before it fires its main rocket engines? I am assuming if the thrust is high enough then the rocket should eventually stop rotating and travel in a straight line. assume the rocket is in a universe without...
Hello all!
Lately i have been looking at many rocket equations, and i was wondering about the gravity loss on a rocket launch. I found the formula for the gravity loss
where g is of course the gravitational acceleration, and y is the flight path angle, but can somone explane why it looks like...
Homework Statement
I am using the NASA CEA code to generate Isp and thrust data for the SSME. I solve the problem twice, once with a frozen flow condition and a second time with an equilibrium flow condition.
However, there is a third request for solving the problem with equilibrium flow from...
hello there
Im trying to do a derivation of tsiolkovsky's rocket equation, but i got stuck at the step when i have to use separation of variables (marked with red in the pic), i used maple to solve it, so i could get on with it, but i want to understand what is happening to solve this, so can...
Hi, here are image of situation. We have observer in point A. He have clock and know distance L between points B and C. He is observing rocket travel from point B to point C at speed near light speed. Can he calculate the speed of rocket using v = L / TimeA?
In rocket at point B here are...
Homework Statement
"Figure 9-55 shows a two-ended "rocket" that is initially stationary on a friction-less floor, with its center at the origin of an x axis. The rocket consists of a central block C (of mass ##m_C=6kg##) and blocks L and R (each of mass ##m_L=2kg## and ##m_R=2kg##) on the left...
Someday, mankind will be able to construct rockets that can move at relativistic speeds.
The acceleration is given by ##a=\frac{F_0}{γ^3m_0}##
##F_0## can be easily measured by placing a force gauge on the rocket itself.
The acceleration is much harder to measure, is has to be measured in a...
Homework Statement
Hi, I would like to apologie for my bad english, but I will try to write my problem as good as I can.
I have a homework...From one stage rocket with initinial speed [m[/0] Ciolky´s number C are escaping gasses with the speed u.
Let´s assume that weight of the rocket is...
A simple problem with a constant acceleration, ignoring mass of the fuel.
The velocity of a rocket, which moves withe a constant acceleration g, is equal:
v(t) = gt
but I want to keep the const acceleration inside the rocket, not in the absolute sense.
An acceleration has a dimension: L/T^2...
Homework Statement
So suppose there is a chemical rocket operating in the vacuum of space (assume it's a perfect vacuum). It generates a hot gas with a total enthalpy of h. What's the final speed of the rocket exhaust, in terms of h?
Homework Equations
The energy equation seems to be useful...
Homework Statement
The figure shows a two-ended “rocket” that is initially stationary on a frictionless floor, with its center at the origin of an x axis. The rocket consists of a central block C (of mass M = 6.40 kg) and blocks L and R (each of massm = 1.90 kg) on the left and right sides...
https://www.sciencedaily.com/releases/2016/09/160929161628.htm
Return trips to Mars without refueling could be a step closer, thanks to a unique new thruster technology.
Homework Statement
To solve this problem you will need to construct a differential equation. A picture of the situation will help. Ignore all gravitational forces. A Rocket ship of structural mass M and fuel mass m, begins at rest relative to a gas cloud. The ship burns fuel at the rate ω which...
just an odd question that passed through my mind when i was watching a SpaceX youtube vid have we (as in humans)ever gotten a rocket to land on the ground with the nose up and the thrusters down (the same position the rocket took of in)?
Homework Statement
Rockets are propelled by the momentum of the exhaust gases expelled from the tail. Since these gases arise from the reaction of the fuels carried in the rocket, the mass of the rocket is not constant, but decreases as the fuel is expended. Show that for a Rocket starting...
Homework Statement
Rockets are propelled by the momentum of the exhaust gases expelled from the tail. Since these gases arise from the reaction of the fuels carried in the rocket, the mass of the rocket is not constant, but decreases as the fuel is expended. Show that for a Rocket starting...
Homework Statement
A rocket sled moves along a horizontal plane, and is retarded by a friction force ##f_{friction} = \mu W##, where ##\mu## is the kinetic friction constant and ##W## is the weight of the sled.
The sled's initial mass is ##M_0##, and its rocket engine expels mass at a constant...
As already posted on PF, and you have likely seen in the news, a SpaceX rocket exploded, September 1, 2016. Elon Musk is reaching out for help in finding out how it happened. http://www.csmonitor.com/Science/2016/0911/SpaceX-needs-you-Musk-calls-on-public-government-in-explosion-probe
I took...
Homework Statement
Force exerted by the ground on the rocket
Mass of the Rocket = 1500kg
Duration of landing impact = 0.04 s
Velocity at time of impact = 175 m/s
Distance traveled = 30km
Time taken to complete journey = 6 minutes
Acceleration due to gravity = 9.8 m/s^2
Homework Equations...
Homework Statement
A 35 m long rocket is receding at 0.6c. From the point of view of a stationary observer, how long does it take for light to travel (a) from the bottom of the rocket to the top and (b) from the top to the bottom?
Homework Equations
t = d/v
L = L0 / gamma
The Attempt at a...
They just lost a rocket:
http://www.bbc.com/news/world-us-canada-37247077']SpaceX[/PLAIN] rocket: Explosion at Kennedy Space Center ahead of launch
http://www.bbc.com/news/world-us-canada-37247077'][/PLAIN]
I was wondering if there is an actual definition given by a recognised organisation over what is meant by the word "rocket". In case there is not, I wanted to reflect upon what do we really mean when we say rockets.
For a highly relativistic rocket powered by an external laser such that the thrust is 2*Power/c, the efficiency is dismal at the start when v is low yet approaches 100% as v approaches c. I take efficiency to mean the ability to convert the energy of the beam into usable kinetic energy. Does the...
Due to the constant never ending supply of "cool stuff" happening in Aerospace these days I'm creating this thread to consolidate posts every time something new comes along. Please feel free to add random information if its relevant. So to start things off here is the SpaceX Dragon launch coming...
Hey guys, I'm trying to write a small article that very simply explains some of the math involved with a rocket engine. I'm not looking for a very accurate answer so I tried the following method
1) Stoichiometry on the fuel which was sugar and saltpeter and their respective enthalpies of...
No question this time, just wanted to share this. I searched the posts and only came up with an eleven year old thread, so I thought it might be time to post a new one. I particularly found the aspect of Methane fuel interesting...
I had someone ask me how rockets are able to accelerate in space and my initial answer was that the rocket fuel combusts and is heated into an energetic gas, the gas is accelerated out of the back of the rocket (i.e. the rocket exerts a force on the gas), then according to Newton's 3rd law, the...
Hello, I was curious about how to calculate how fast the escape velocity of hydrogen out of a tube/cylinder would be. Once end of the cylinder is closed, the other is open, obviously.
Assume the cylinder is full of hydrogen at 1 atm. My thought is that you could use PV=NRT to calculate the...
Homework Statement
I am going to paste the problem word for word, so you can have all the exact information that I have:
You’re part of a team that’s designing a rocket for a specific mission. The thrust (force) produced by the rocket’s engine will give it an acceleration of a feet per second...
Hello! I am predicting the peak altitude of a model rocket based on some ground tests. I know that Total Force on the rocket=Thrust-mg-kv^2 but am stuck as to which value for 'v' to use? Is it the velocity of the rocket with the effects of gravity and air resistance taken into account or the...
I was debating with a friend, who insisted that the thrust in a rocket is merely due to the fact that a force PxA would have acted on a plate that sealed the nozzle. This force would have exactly balanced its counterpart "disk" on the other side of the chamber. After removing the seal, we are...
Hello everyone,
I am predicting the altitude of a model rocket based on some testing I did where I found the impulse of a little single stage model rocket motor. I am wondering how to incorporate drag into my calculations to make it more accurate. I know D=Cd*rho*v^2*A and I can definitely find...
Hello all.
In Morin's classical mechanics book, chapter 12 (relativistic dynamics), in the axample about the relativistic rocket, we have a rocket that propels itself converting mass into photons and firing them back. Here Morin takes dm as a negative quantity, so the instantaneous mass of the...
So I was wondering how come liquid rocket engines (operating in the lower atmosphere (such as launch stages)) are using Oxygen that they have packed on board. What I mean to say is why would the rocket need to waste space and mass bringing Oxygen with them in the launch stage when they could...
Homework Statement
A rocket starts at rest from the Earth, moving in the z direction so that in its own instantaneous rest frame the acceleration is always g = 9.8 m/s^2. To an observer on Earth, its position is given by
## z(\tau) = \frac{cosh(g\tau) - 1}{g} ##
## t = \frac{sinh(g\tau)}{g} ##...
Is there any equation in order to know how high my rocket will go, before launching it? I suppose that if there is any, it will not take into account air drag and others, and there is no need for that. I just one to know an approximate, I am making a summer project with some friends and we had...
Hello everyone. I want to be interest in rockets. How I begin? Which books are I have to read? I'm also interesting with aircraft. Especially unmanned aircrafts. I have a little bit aerodynamic infrastructure. I'm waiting your answers. Thank you.
For an agency can a physicist be employed as a rocket scientist or he has to get a degree in engineering?
If not does he need to take some special courses to convert himself to a rocket scientist?
Hey,
Suppose you have an enclosed vessel that is full of water. You heat it up then you open a valve, and that will create enough thrust for it to act as a rocket.
How much energy is needed for a steam rocket to get heated enough to achieve a mass flow rate of 2430 Kg/s.
Mass of water= 256...
The USN used to shoot ASROC from box launchers. It was a torpedo with a rocket motor on the back. it was ballistic. The rocket fired and then separated mid flight. the torpedo continued on, a chute was deployed to slow and I think stabilize the water entry after which the torpedo went on...
Hey folks. I've done a little bit of research into model rocketry and I'm stuck with the idea of designing and projecting a rocket to put into practice all the engineering I'm learning in college - I'm into MechE. I want to start simple, doing a few tests and learning the basics - types of...
Homework Statement
A railroad car moves under a grain elevator at a constant speed of 4.50 m/s. Grain drops into the car at the rate of 420 kg/min. What is the magnitude of the force needed to keep the car moving at constant speed if friction is negligible?
Homework Equations
U=V+dV-Vrel , U...
Hello Forum,
For a combustion to happen, there needs to be one material that plays the role of the fuel and another material that is the oxidant.
For example, fuel and oxygen react together to produce light and heat and expanding gases.
In making rocket fuel, sugar is used as fuel and...
Had been talking NSWRs on a spaceflight forum and a thought occurred to me. Lithium-6 fission can be triggered with relatively low-energy neutrons and releases 4.78 MeV, a helium-4 atom, and a tritium atom. Without a neutron flux, however, lithium-6 is completely stable.
With a small...
Homework Statement
Rocket is accelerating constantly. Let S' be instantaneous rest frame of rocket and S be frame in which rocket is observed moving at velocity v.
Homework Equations
Given: $$ dv = dv' (1 - v^2) $$
Must prove:
$$ \frac{dv}{dt} = \frac{dv'}{dt'} (1 -...