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
Earlier we considered a rocket fired in outer space where there is no air resistance and where gravity is negligible. Suppose instead that the rocket is accelerating vertically upward from rest on the Earth's surface. Continue to ignore air resistance and consider only that...
Homework Statement
This is from chapter 1 (2nd edition) of Taylor and Wheeler's 'Spacetime Physics.'
It's a four part problem, and I didn't have any troubles with parts a, b, or c. I'm stuck on part d. I'm supposed to determine if we could make it to Andromeda within a lifetime.
Assume that...
Homework Statement
A manned expedition is planned to be sent to Mars in 2023, one way. If the colony module was 100.0 tonnes in mass. Determine the work that must be done by the rockets to carry this colony from Earth to the surface of Mars.
Homework Equations
ET = PE +KE
PE = -GmM/r
KE =...
Homework Statement
I'm having trouble deriving the equation for the velocity of a rocket in constant G given that it has constant exhaust velocity
Homework Equations
I know that a=dv/dt=U/M(dM/dt)-g
The Attempt at a Solution
so from here dv=U/M dM-gdt
v=U ∫1/M dM - g ∫dt v from 0...
Homework Statement
A rocket is launched straight up with constant acceleration. Four seconds after liftoff, a bolt falls off the side of the rocket. The bolt hits the ground 6.0s later.
Homework Equations
v_x = v_0 + at
x_f = x_0 + v_0t + 1/2at^2
v_x^2 = v_0^2 + 2a(Δx)
The Attempt at a...
Homework Statement
A "rocket car" is launched along a long straight track att = 0 s. It moves with constant acceleration a1 = 2.9m/s2 .At t = 2.8s , a second car is launched with constant acceleration a2 = 7.0m/s2 .
At what time does the second car catch up with the first one?
How far down the...
What do you guys think about the recent vote where the house of reps decided to ban (100-300 or so) imports of these Russian rocket engines? Seems like politicians and corporations looking to make a buck (like SpaceX) have succeeded in their lobbying for the ban on RD180 engine import. Is it OK...
I am stuck on how my teacher got to the last equation in #4.
Problem Statement:
A 2,000 kg rocket carrying 3000 kg of fuel is drifting in space when it fires its engine. While operating, the rocket engine burns 20 kg of fuel per second and the exhaust gasses leave the rocket at an exhaust...
Hello,
I've always been interested in space and space flights and have often wondered how rockets are lunched into space, how their trajectories are defined, how they are sped up (like gravity assist), how they are slowed down (like the complicated trajectory of the Rosetta mission etc . . .
I...
Hello, I am new here and I would like to know if anyone on here can answer a question for me. How far could a saturn V rocket (http://en.wikipedia.org/wiki/Saturn_V) push comet 67p off course if it were 100 million miles away? Also, how long would it take this rocket to stop the comet if it...
Homework Statement
A rocket through interstellar dust, no gravity. Solve for v with respect to mass.
k is a constant.
Drag = -bv
Homework Equations
[/B]
The Attempt at a Solution
To start:
It should become a separable differential equation, but I am having a lot of trouble solving it...
Carolynne Campbell, a rocket propulsion expert based in the Netherlands said that multiple warnings about the spacecraft s motor and fuel had been issued to Virgin since 2007. " I warned them that the rocket motor was potentially dangerous " Her warnings were related to the nitrous oxide and...
Okay, first of all, I'm not very good at maths, so I will have to talk in programmer terms here. I have the following issue:
A small rocket is moving in space, and I want it to move to and stay at a location in space, similar to a quadcopter.
No as far as I see it, I have the following variables...
Homework Statement
How does change the total energy of the rocket during its motion inin a uniform gravitational field?
2. The attempt at a solution
My idea is to write the law of conservation of energy systems - "rocket- gases" ##\frac{dE_{total}}{dt}=0##
But get very cumbersome terms , the...
well. I have this question. That my rocket is launched from mar in an return mission to earth. To calculate specific impulse of the rocket. Should i consider mar or Earth gravity and if why!? Help me with this
Hi i am doing a project on the future of solar energy. While reading up on rockets and how they are propelled to escape velocity i noticed all references only tell us that the hot gases propel the rocket up. Could someone explain exactly how this happens. What i mean is does molecule collision...
I have noticed many of the thrust derivations in textbooks I have seen do not do a straightforward derivation of rocket thrust. The all seem to use the same trick with infinitesimals in a sort of binomial form. For reference:
Taylor, "Classical Mechanics" Pg. 85.
I am working on a rigorous...
Homework Statement
A rocket is initially at rest on the ground. At time = 0, its engines ignite causing the rocket to move in a straight line with constant total acceleration of a = 30 m/s^2 at an angle of 76 degrees, and the engines are strong enough to counter gravity and keep it exactly in a...
Background
This is for a video game, "Kerbal Space Program"... I'm sure some of you here have heard of it. It's the type of game you guys would be interested in.
I have built a program to design rockets, but I'm not sure what the optimal thrust-to-weight ratio is. That is, how much fuel I...
Homework Statement
A single-stage rocket is in deep space coasting at vrocket,i = 2.4 × 103 m/s. It fires its engine, which has an exhaust speed of vexhaust = 1.3 × 3 m/s.
What is the rocket's speed vrocket,fafter it has lost one-third of its inertia by exhausting burned fuel? Assume that the...
Homework Statement
A) A rocket fires two engines simultaneously. One produces a thrust of 675N directly forward while the other gives a thrust of 450N at an angle 20.4∘ above the forward direction.
a) Find the magnitude of the resultant force which these engines exert on the rocket...
Homework Statement
A rocket with a mass of 7.2 x 10^4 kg starts from rest in outer space and fires its thrusters until it is moving with a velocity of 100 m/s. What was the average force on the rocket due to the thrusters?
Homework Equations
1/2 mv^2 = Fxd
The Attempt at a...
... Continued from part 3.
The Sands of Duna
Part 4: We have ignition
The author of this post (and story), collinsmark, is not affiliated with Squad nor Kerbal Space Program.
We've waited long enough. So let's get this ship out the launch pad.
Kerbals chosen for this mission are
Melmon...
Which are more efficient, Rocket Engines or Jet engines, and why? It would make sense that rocket engines are more efficient because they aren't effected by air pressure but I have been told by some people that actually Jet engines are more efficient so I am confused. If you know of any link...
I’ve been thinking about Einstein’s gedankenexperiment (because I’m meta like that) regarding the sealed room on Earth, and the sealed room on a steadily accelerating rocket. And the result of this thought process is… I’m confused, probably because I do not correctly understand the parameters...
Homework Statement
A rocket is moving in a gravity free space with a constant acceleration of 2 m/s2 along + x direction (see figure). The length of a chamber inside the rocket is 4 m. A ball is thrown from the left end of the chamber in + x direction with a speed of 0.3 m/s relative to the...
The Little Rocket That Could
[Figure 1. Check this out.]
This post illustrates an example of KSP rocket design. The following are the rocket's design goals:
Get three kerbals and a bunch of science items to the Mun, in an Apollo style mission: such that two kerbals (and science) land on the...
The concept of a problem is that if rockets continue to jettison fuel, at some point they will get a very small momentum because their mas will be so small. (Bit of a silly problem, there's a lot of mass in the rocket itself) Anyways, the idea is that you would take the derivative of the...
Having some trouble with this problem.
I'm not sure if the first part is correct, I just need some feedback on that.
Also I'm not sure how to calculate velocity or altitude after 1 second.
Any help would be awesome!
Homework Statement
A rocket has an initial mass of 4000kg, of which 3000kg is...
Homework Statement
A rocket is launched such that when the fuel is exhausted, the rocket is moving with a speed of Vo at an angle of 37° with the horizontal and at an altitude h. (a) Use energy methods to find the speed of the rocket when its altitude is h/2. (b) Find the x and y components of...
In AP Physics B, for our physics olympics, for one event, we are required to make a paper rocket that will be launched straight up in the air by an air compressor and pump. (60 psi)
We have already assembled the paper rocket, with one cylinder of paper, a cone paper nose, and a load of tape to...
I have a question regarding the design of rocket nozzles. I am not an engineer nor a physicist but I am involved in amateur experimental rocketry and I was curious regarding grossly overexpanded nozzles.
According to Wikipedia a grossly overexpanded rocket nozzle (very bottom of the...
Homework Statement
Consider a rocket making a vertical ascent in a uniform gravitational field, g. Show that the height of the rocket when the fuel is exhausted is given by
x = ut_b - \frac{1}{2}g{t_b}^2-\frac{um_R}{α}ln{\frac{m_R+m_F}{m_R}}
where "u" is the exhaust velocity of the fuel...
i was wondering why not use the air in the surrounding to oxidise the fuel in the first stage of a rocket? it definitely will burn with the fuel(assuming bi propellant ) and will also reduce the wet mass of the rocket? is there any problem with this ?
Given an ideal rocket in a friction-free, gravity-free environment:
A precise amount of energy E is applied to accelerating a rocket. An external observer at the origin (rocket velocity=0) watches the rocket accelerate to a final velocity V. As expected, the origin observer finds that V...
Homework Statement
Interstellar Spaceship
An interstellar spaceship with initial mass Mo is at rest at the edge of a small, spherical nebula (gas cloud). At t= 0, the engines begin to fire, ejecting gas out the back at constant speed u relative to the rocket. The mass of the rocket decreases...
Hello
Firstly i just registered, I am a final year computer science student and I am busy working on my thesis (the deadline is fast approaching) I am working this application of a rocket going into orbit and physics is not my forte. I need some help on converting the gimbal of a rocket...
Hi all!
I have entered a a water rocket competition. The rockets in this competition will be launched at 60 psi. We have to launch the rockets horizontally and to hit a round landing site 100 meters(approximately 328.084 ft) away and 30 meters (approximately 98.4252 ft) wide. I am not good at...
Homework Statement
A rocket of length ##L_o## flies with constant velocity ##v## (in frame S' relative to a frame S in the x direction). At time t=t'=0, the capsule on the top of the rocket passes the point ##P_o## in S. At this moment, a light signal is sent from the top of the rocket to the...
I'm trying to calculate the thrust produced by a steam rocket, but I don't have that much information to work with (or at least information I don't know what to do with). It's 2m long and has a diameter of 1m, and it's constantly filled with water at a rate of 170.344L/sec, which is...
A rockt with mass \(M\) is sitting motionless in space. The rocket is powered by steam with velocity \(V_s\) and mass per time \(C = \frac{dm}{dt}\). Write an equation for the rockets acceleration in terms of \(M, {} V_s\), and \(C\).
So \(\mathbf{F}_s = \mathbf{F}_r\) by Newton's 3rd. By...
Homework Statement
a rocket explodes in flight into two equal mass pieces still going in the same direction with one piece moving twice as fast as the other. What is the ratio of the total kinetic energy of the pieces just after the explosion to that of the rocket just before?
Homework...
Homework Statement
A model rocket is launched with an initial velocity of 55 m/s. Its height as a function of time can be modeled by h(t) = -4.9t2 + 55t. Determine the maximum height reached by the rocket.Homework Equations
h(t) = -4.9t2 + 55tThe Attempt at a Solution
h'(0) = 55, since h'(t) =...
My first post, and a very long one...
I have problems understanding the prolific use of a certain term in the rocket thrust equation and its validity.
The general rocket thrust equation contains a term referred to as the pressure thrust. It is calculated as (p_e – p_a)Ae where p_e is the...
Hey everyone, so I'm just wondering if you guys can articulate the term "velocity of lost mass" from the rocket. After a few massaging on the equations(derivatives and integrals stuff) i found that to manipulate the thrust, one must manipulate the burn rate AND the "velocity of loss mass". all i...
A test rocket is launched, starting on the ground, from rest, by
accelerating it along an incline with constant acceleration a. The incline has length
L, and it rises at θ degrees above the horizontal. At the instant the rocket leaves the
incline, its engines turn off and it is subject only...
Homework StatementA rocket is accelerated for 10 years at a constant rate of 10 m/s². Then starts braking at -10 m/s². Then goes all the way back to its starting point by again first accelerating 10 years at 10m/s² and then braking at the opposite rate for 10 years. How much time has it been for...
Homework Statement
I am trying to model a water rockets motion using a computer programme in order to compare it to my experimental data. I am studying physics at degree level but I have no knowledge of programming and am finding this particularly difficult. I have thought about using...
hello guys
could anybody tell me the method of finding the range of a rocket launched from height h,
the rocket of course is under three forces weight,drag and thrust