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.
I made up a scenario: Let's say I have a rocket at rest in space. The rocket initially weighs 100 kg, 50 kg of which is fuel. If the fuel burns at a constant rate of 1 kg/s and produces a thrust of 100 N out the back of the rocket, what will the rocket's velocity be after it runs out of fuel...
Homework Statement
given a graph of the thrust of an engine, we need to determine what mass to make our rocket so that it goes 15m into the air. Here is the graph:
http://www.321rockets.com/content/image/26402/800/A8_thrustcurve.jpg
I just need some confirmation on if I'm doing it right...
Rocket Project -- need to find mass of rocket to reach 15 m altitude
I have a project for grade 11 physics, i have to create a rocket that reaches precisely 15 m altitude, and all I am given is the thrust profile of the engine (force(N) vs time(s) graph)
It is an Estes A8-5 engine
i have...
A rocket, which is in deep space and initially at rest relative to an inertial reference frame, has a mass of 59.5E5 kg, of which 7.39E5 kg is fuel. The rocket engine is then fired for 300 s, during which fuel is consumed at the rate of 480 kg/s. The speed of the exhaust products relative to the...
I am a high school teacher attempting to give my students a project for designing a rocket powered by the chemical reaction between acetic acid and baking soda to produce CO2 gas.
I have done some simple calculations based on stoichiometric amounts of vinegar and acetic to produce a...
Homework Statement
A 1200 kg rocket car is placed at the bottom of a 100 meter long ramp inclined at 10°. The rocket is turned on and it exerts a force of 8300 N for 5.70 seconds, and then it shuts down. Find the speed with which the rocket car leaves the ramp (assume frictionless)...
I am building a liquid fueled rocket engine driven gas generator. I plan to use gasoline for fuel and oxygen gas at a rate of .022lb/sec and O2 at .055lb/sec The chamber is 2.15 in long 1.15 in id with a .238 nozzle. The chamber pressure should be 300 psi with a thrust of 20 pounds. I calculate...
Homework Statement
A rock of blasts of vertically from rest on the launch pad with an upward acceleration 2.60 m/s^2= At 30s after blast off, the engine suddenly fails, which means the force they instantly stops.Homework Equations
The Attempt at a Solution
How high above the launch pad will...
The set up:
A 20,000kg rocket has a motor that generates a thrust of 3x10^5 N.
The problem:
a)What is it's initial Acceleration?
b)At an altitude of 5,000m the rockets acceleration has increased to 6 m/s^2, what mass of fuel has it burned?
Relevant equations:
F = ma
The...
Rocket travels into space, emits sound -- intensity/time question
Homework Statement
A rocket, starting from rest, travels straight up with an acceleration of 56.7 m/s2. When the rocket is at a height of 722 m, it produces a sound that eventually reaches a ground-based monitoring station...
Homework Statement
Please check my work
A model rocket is launched vertically upwards with an initial speed of 50m/s. It accelerates with a constant upward acceleartion of 2m/s until its engine stop at an altitude of 150m.
2.4.1) What is the maximum height reached by the rocket...
Take a typical single-stage rocket that reaches low Earth orbit (that's around 2000 km).
How much fuel is burnt just to get the thing a foot off the ground? Or a kilometer or a mile? 10%?
Homework Statement
In the first stage of a two-stage rocket, the rocket is fired from the launch pad starting from rest but with a constant acceleration of 3.50 m/s^2 upward. At 25.0 seconds after launch, the second stage fires for 10 seconds, which boosts the rocket's velocity to 132.5m/s...
A rocket starts from rest and moves upward from the surface of the earth. For the first 10 of its motion, the vertical acceleration of the rocket is given by 2.60t, where the -direction is upward.
What is the speed of the rocket when it is 240 above the surface of the earth?
v = v0 + at...
An ice sled powered by a rocket engine starts from rest on a large frozen lake and accelerates at +38 ft/s2. After some time t1, the rocket engine is shut down and the sled moves with constant velocity v for a time t2. Assume the total distance traveled by the sled is 15750 ft and the total time...
Homework Statement
Studying Special Relativity at the moment, and having a little trouble getting to grips with it. I've got stuck on this question, and was wondering if anyone could clear it up for me?
Here's the question:
"A rocket is traveling at 0.6c, v, along the x-axis relative to you...
Homework Statement
The problem was asking to find the time dilation of a rocket traveling upwards at 100,000 m/s with the reference point being Earth for a duration of a day.
Homework Equations
1/√(1-(β^2))
Δt = γΔt'
The Attempt at a Solution
I've calculating gamma to be...
Homework Statement
A rocket of initial total mass mi leaves a space station in deep space, far from all sources of gravitation. The rocket ejects burn fuel at a constant speed u << c relative to the rocket.
(a) Derive an expression for the rocket relative to the space station when the...
Why aren't helium balloons used to carry rockets or payloads to the troposphere which is about 25km above sea level before they are launched?
To reach actual outer space is 100km above sea level. The above will in turn save 25km worth of fuel and the overall mass of the rocket which needs to...
Jetpack International's T-73 achieves vertical takeoff with an actual jet engine as opposed to the rocket engines used by the majority of jetpack models. This allows it to have longer flight time (9 minutes as opposed to 30 seconds). Some fighter planes also manage VTOL with a jet engine, the...
When combustion occurs in a rocket engine, most of the high speed fluid passes out the back as exhaust. But surely some of it flows back through the fuel and oxidizer injector tubes? Wouldn't this decrease efficiency (and potentially even lead to safety risks)?
Homework Statement
#1.) A rocket exhausts fuel with a velocity of 1500 m/s, relative to the rocket. It starts from outer space with fuel comprising 80 per cent of the total mass. When all the fuel has been exhausted the speed is...
(Answer was 2400 m/s)
Homework Equations
Vrel...
Homework Statement
In this thread the author performs the following calculation under "method 1":
v+dv=\frac{v+dv'}{1+vdv'}=v+(1-v^2)dv'\implies dv'=\frac{dv}{1-v^2}
He's set c=1 so the second expression is the relativistic velocity addition formula. What I don't understand is how he gets the...
Homework Statement
A rocket is accelerating vertically, and it is ejecting gas downwards (which allows it to move upwards) at a rate of B. The gas is ejected at a velocity w relative to the rocket.
What is the velocity and acceleration of the rocket as a function of time?
Homework Equations...
How would the equation look if instead of knowing the effective exhaust velocity we knew the force the exhaust was exerting on the rocket.
The equation is:
\Delta V = v_e * ln(\dfrac{m_0}{m_1})
would \Delta V still be proportional to the log of the initial mass over the final...
Homework Statement
A 20,000 kg rocket exhausts gasses at a constant 700 kg/sec at 300 ms^-1
Deduce the thrust applied to the rocket by its engines
Homework Equations
The only equation I know is a= T- mg/m
Where T= thrust
a=acceleration
m=mass
The Attempt at a Solution
I don't...
Q: The motors of a 1,000 kg rocket standing vertically on the ground are being tested. Fuel is being burned at the rate of 5.0 kg/s with an exhaust speed of 2.8 km/s. Find the force needed to hold the rocket down.
Attempt: I'm not really sure how to go about this question. I've thought about...
We all know that any biological or an other chemical activity occurring inside a rocket traveling at 0.8c appear to be slower to an external observer.
Then the rate of combustion of fuel in the rocket should also be reduced according to that.
Then what prevents the rocket from slowing down...
Homework Statement
A rocket with mass 60 x 103 kg (25 % of it is "empty mass"). The rocket burns the fuel at rate 250 kg/s and expel the gas at relative speed 1.6 km/s. Find the force experienced by the rocket and the time until the force equals to zero
Homework Equations
Δp = F.Δt
p =...
Homework Statement
A rocket launched vertically takes 6.13 seconds in total. How much time does it take the rocket to reach its maximum height. What is the velocity of the rocket in meters per second at maximum height? What is the initial velocity of the rocket. Give your answer in meters per...
The burned gases of a rocket engine are ejected from the rocket nozzle at a speed of 17,000 ft/sec. If the weight of gas ejected is one pound per second, find the thrust developed by the rocket.
I don't really have an equation to use here but my guess is F = M\32.2 * Ejection Velocity...
Homework Statement
Calculate the final velocity of a rocket if the velocity of the ejected gas is c, initial mass of rocket is M0 and final mass is Mr, v0=0.
Homework Equations
We have to calculate the final velocity of rocket.
The Attempt at a Solution
Because the total momentum...
Homework Statement
The following equation is known as the "Rocket Equation":
\frac{M+P}{M}= e^{ΔV/C} = mass ratio
M = dry mass
P = mass of propellant
C = exhaust velocity
ΔV = velocity changee^1 = 2.72
e^2 = 2.74
e^3 = 20.4
As ΔV/C goes up, the mass of the spacecraft goes up faster...
I have been thinking, weather balloons can go quite high (some up to 1000ft) so would it be possible to take 4 or 5 weather balloons and attach them to the corners of a frame. in the centre of the frame would be a rocket ready to launch at a set altitude. the only problem i can think of is...
Homework Statement
Ok, the problem says some rocket of mass M0 has this new technology that allows it to convert photons into fuel. It reaches a speed of .5c. The problem asks us to solve for the final mass of the rocket, and then assume that all the lost mass was converted into photon fuel...
Hello everyone,
Over the past year, I have been trying to simulate the launch of a rocket to orbit using excel. I have been pretty successful, and I have what I think to be a mostly working product. However, it has some problems that may be affecting the results.
First, I'l explain roughly...
Homework Statement
A 2.45×10^4-kg rocket blasts off vertically from the Earth's surface with a constant acceleration. During the motion considered in the problem, assume that remains constant. Inside the rocket, a 13.1-N instrument hangs from a wire that can support a maximum tension of...
Homework Statement
The mass of a rocket as it burns its fuel is constantly decreasing, while its speed is increasing. We want to know when the momentum is at its maximum. At what fraction of the initial mass is the momentum a maximum?
Homework Equations
P = mv
The Attempt at a...
A small rocket powered by high-pressure nitrogen (R = 1776 ft-lb/slug/R, gamma=1.4) is used as an attitude control device. In space, the thrust of a rocket is given by T =mVe
in lbf. Find the thrust and exit diameter of this rocket with a throat diameter of 1.0 inch if it
operates at PT =...
Question about the a "relativistic rocket"
Intro:
If one was to measure the redshifts and distances of all galaxies around earth, they would come to a conclusion that they were in the center of the universe because all the galaxies are "moving away from them" faster as the distance to them...
Homework Statement
Suppose a rocket is launched from the surface of the Earth with initial velocity
v_0 = \sqrt(2gR) , the escape velocity.
a) Find an expression for the velocity in terms of the distance x from the surface of the Earth (ignore air resistance)
b) Find the time...
This is an even numbered exercise so I am not able to get confirmation from the book on the correct answer.
Homework Statement
An observer in a rocket moves toward a mirror at speed v = .8c relative to the reference frame S. The mirror is stationary with respect to S. A light pulse emitted...
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 s along its initial straight line of motion with an acceleration of 30m/s^2. FInd the max altitude reached by the rocket
Homework Equations
y=y0...
Having a little trouble with this latest advanced egg drop assignment. The main assignment has two parts -
1. Create a rocket that can reach a minimum height of 120 ft
2. Create a vehicle that can land with an egg for a passenger, and not have it crack.
We also aren't allowed to use...
Hi all,
I had an exhaustive time looking on the web for software (either free or commercial) that allows someone to simulate trips into the solar system from planets. I'm looking for something that can simulate spaceship flybys in Hohman Transfer Orbits, Gravity Assists, Oberth Effects...
Homework Statement
A rocket is launched at an angle of 53° above the horizontal with an initial speed of 75 m/s. It moves in powered flight along its initial line of motion with an acceleration of 25 m/s^2. At 30 s(seconds) from launch, its engine fails and the rocket continues to move as a...
Hey everyone,
I've been trying to do a problem in which I attempt to find the angle that maximizes the horizontal distance of a rocket, which has a stage with thrust and then a stage as a projectile. After a delay period, an ejection charge fires and causes the rocket to drop straight...
Homework Statement
A rocket is launched at a planet of 600km radius, 5.29e22 kg mass, and 9.8068 m/s^2 surface gravity such that it reaches a maximum height 'h' with work 'x'. What is the value of 'x'? Ignore air resistance, and gravity is dependent on height.
Homework Equations
Unsure of...
Homework Statement
A model rocket is launched from rest with an upward acceleration of 6.00m/s^2 and, due to a strong wind, a horizontal acceleration of 1.50m/s^2. How far is the rocket from the launch pad 6.00s later when the rocket engine runs out of fuel?
Homework Equations
Not sure..The...