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'd always thought that to find the mass ratio of a given rocket, one simply had to divide the rocket's wet mass (i.e. fuel and propellant) from its total mass. An example: a rocket's total mass = 2,000 tonnes: its wet mass = 1,000 tonnes. Answer: 2. Is this correct? (I'm pretty sure it isn't...
'allo!
I am currently a 10th grader trying to make a resistojet for a science project in an attempt to find out which heating filament geometry makes the resistojet most efficient (if changing the shape changes performance at all). A resistojet is a mode of propulsion that uses resistive...
Homework Statement
A rocket during launch from the Earth's surface moves vertically with an acceleration of 22m / s ^ 2. Find the cosmonaut's weight inside the cabin if his mass is 90kg.
Homework Equations
The problem belongs to "Elasticity. Moving under the action of elastic force" chapter...
Greetings All!
I am not sure if this is the correct place to post this, but I think that since rocket fuel is considered a chemical reaction, this sections seems appropriate. Right, to the topic. Me and my team from the spaceflight society are looking forward to building a hybrid rocket fuelled...
I have been working on a rocket engine and I have cad models and everything and I am getting ready to build it. Then, I was running over the numbers one more time and I realized that the thrust I was getting was completely different from what I should have been getting.
The big problem is the...
Homework Statement
We are doing water rockets and I don't know how to calculate the height it went from it's hang time. It's total hang time was 7.35 seconds, and I know it's vertical acceleration was -9.8m/s^2 from gravity, and I'm assuming I need to first find out it's initial velocity, since...
Homework Statement
A rocket has weight 10,000 kg and it needs to carry 5000 kg with acceleration 3.5 m/s². How much thrust force is necessary for the rocket to have a flight from Earth to space?
Homework Equations
F=ma[/B]The Attempt at a Solution
I try that, According to Newton's law, (...
Hey Guys,
I'm on a rocket team at my university and we are attempting to figure out the force of opening acting on some of our parachutes. Typically this is done using the following equations, in particular, the one in the top right corner.
This is where our trouble begins. In the Recovery...
I gather rocket energy efficiency is maximal when exhaust speed closely matches the rocket speed (but oppositely directed), so to an outside observer such a rocket would leave a stationary propellant trail. I’ve found little on this model and am trying to learn more.
Say we have a rocket of...
110kg sounding rocket that runs on apcp
im trying to understand the steps to building this rocket what equations do i use to find nozzle parameters and estimated burn time etc. initial surface area for the fuel block is 5020cm^2
burn rate is .6 to 1.2mm a second fuel weight is 100kg gamma for...
So I was browsing wikipedia when I encountered:
What does this exactly mean? How does one calculate for this?
<< Adding link to the table >> https://en.wikipedia.org/wiki/Spacecraft_propulsion#Table_of_methods
I was assuming that the proper time lapse between ##r=2M## and ##r=0## increases with increasing acceleration outwards.
According to this paper
https://arxiv.org/pdf/0705.1029v1.pdf Fig.2.
it turns out however that the proper time to reach the singularity is longer with low acceleration but...
Hello, PF. So I was wondering if it's possible to power a spaceship by solar power only. If so how big will the solar panels be? Where would they be installed? How long will it take for them to fully charge in order to travel a certain distance? between Earth and the moon for instance.
Homework Statement
The 13-kN rocket sled is propelled along a straight test track. The rocket engine fires for 4 seconds,
producing a propulsive force of F=5.3kN, and then shuts down. Assuming that the sled starts from rest and that the coefficient of kinetic friction is 0.05, determine the...
Homework Statement
A 2000-kg is launched vertically from the surface of the earth. The engine shuts off after providing a constant propulsive force of 60 kN for the first 20 seconds. Neglect the reduction in the mass of the rocket due to the burning of the fuel and the variation of the...
Can someone clarify this for me-- how is the motion of the center of mass unaffected by internal forces, as is stated towards the end of the paragraph in the picture I've provided. It seems to me that motion of the center of mass directly affected by these internal forces. Specifically, the...
Homework Statement
A two-ended "rocket" is initially stationary on a frictionless floor, with its center at the origin of an axis. The rocket consists of a central block C (of mass M=6 kg) and blocks L and R (each of mass m = 2 kg) on the left and right sides. Small explosions can shoot either...
if you and your friend ride a supersonic rocket , do you can listen to your friend voice ?
I mean if you travel faster than sound will you can hear anything ,It's difficult to imagine.
And thanks so much,
Hi - I just thought of a (relatively) simple example: Here is the problem I can't solve due to my disability to integrate the resulting equation:
I thought about a rocket that gets accelerated by a constant force F... Since the rocket is burning fuel and therefor losing mass at a conatnt rate...
Problem statement:
A rocket propels itself rectilinearly by giving portions of its mass a constant (backward) velocity ## u ## relative to its instantaneous rest frame. It continues to do so until it attains a velocity ## v ## relative to its initial rest frame. Prove that the ratio of the...
Hello! I'm currently in 7th grade, and I want to become a Rocket Scientist. Is there any possible way that I could speed this process up before I take AP tests or CLEP tests or go to college? I know it will be hard, but I want to learn. I think it might have something to do with Linear Algebra...
This is my first post. I looked through many threads and could not find an answer to the question below.
Well known equations in rocketry are:
Delta Velocity = Ejection Velocity * ln (Final Mass / Initial Mass )
and
Net Thrust = Mass Ejection Rate * Ejection Velocity – Current Mass *...
Homework Statement
A 300 g rocket is on a cart that is rolling to the right at a speed of 2 m/s. The rocket engine, when it is fired, exerts an 6 N thrust on the rocket. Your goal is to have the rocket pass through a small horizontal hoop that is 18 m above the launch point. At what horizontal...
A rocket flies past the me with velocity ##0,866## c, therefore ##\gamma=2##. Its length in rest is 10 m. When I am parallel with the last part of the rocket, the rocket stops immediately. The last part stays parralel with me, but the beginning of the rocket jumps for factor 2, therefore jumps...
I have a project where I will be launching a rocket from a high altitude weather balloon. I am planning on launching the rocket at around 70Km or even higher. My main concern is the igniter not being able to ignite the engine because of the low amount of oxygen. Is there any way around this...
Well, first thing, I am new to this forum and it looks pretty good and I'm looking forward to reading more from it and post more questions.
Well rocket propeling (or anything that uses some material to propel up when shooting it down) seems pretty straight forward at first, you have some gas...
Homework Statement
A rocket engine takes 8 seconds after firing to reach its full thrust. Assuming that
the rocket was fired at t=0, use the following time-elevation data to estimate the
velocity and acceleration (a) at t=0; and (b) at t=8s
Homework EquationsThe Attempt at a Solution
I don't...
I want to strap an estes b4-4 rocket to a toy car and calculate how far it would travel.
What I know:
Mass of car: 300 grams
Rocket nominal force: 12.8 Newtons
I think this means the rocket would accelerate my car for a=F/m = 12.8 kg * m/s^2 / 0.300 Kg which means 12.8 m/s^2/ 0.3 = 42.67...
I ran into the Sea Dragon Rocket that was cooked up on paper in 1962, could this have worked efficiently and if so could it have made it to where we would have been much further along in manned space and the ability to launch over sized payloads...
Thanks...
Hello everybody!
I have been thinking about something for a while now. I would like to make a magnetic nozzle for a rocket engine. Basically, I would like to ionize the hot and high pressure gaz in the combustion chamber and then use a strong magnetic field to adjust the nozzle throat...
Homework Statement
Homework Equations
conservation of momentum
Thrust of rocket engine = -u (dm/dt)
u is the velocity of the gas being expelledAlso found this from Wikipedia, not sure if it is relevant
The Attempt at a Solution
For these kinds of problems I assume you need to apply...
I'm going to make a water propelled pop bottle rocket for a competition. The bottle holds 1.5 liters and we are going to fill some amount of it with water and pressurize it to 75 psi. When triggered, water will come out of the hole in the cap and propel the rocket. The rocket is perfectly...
Homework Statement
A 11.6 kg weather rocket generates a thrust of 200 N . The rocket, pointing upward, is clamped to the top of a vertical spring. The bottom of the spring, whose spring constant is 580 N/m , is anchored to the ground.
Initially, before the engine is ignited, the rocket sits at...
Homework Statement
The gravitational potential energy of a certain rocket at the surface of the Earth is -1.9x10^12 J. The gravitational potential energy of the same rocket 300km above the Earth's surface is -1.8x10^12 J. Assume the mass of the rocket is constant for this problem.
A) How much...
Following scenario:
A rocket measuring 10 lightseconds in length accelerates near instantaneously to v=0.4c. Pre-acceleration two clocks placed at the endpoints of the rocket were synced.
What will be the time difference between the two clocks post acceleration?
I tried to figure it out...
Hey guys,
I'm new to the forum and I have a question that has stumped several of the professors at my school. My idea is to use an electric motor with a solid rocket engine on a thrust stand to spin the exit cone. The concept would make use of centripetal force to increase the pressure of...
Homework Statement
A fireworks rocket is launched vertically upward, and explodes into two equal-mass pieces at the top of its trajectory. The pieces hit the ground at t1 and t2 seconds after the explosion. What is the rocket’s launch speed? Assume no air resistance.
Homework Equations
v1 =...
Hello,
I am stuck on a Java problem in my textbook. Can anyone help me? I have tried many variations to no avail thank you.
Question:Write code that prints: userNum ... 2 1 Blastoff! Your code should contain a for loop. Print a newline after each number and after Blastoff!. Ex: userNum = 3...
Based on my current understanding of the problem I do not see this following derivation as valid, although this is what was given in my course notes. Although this particular example is from an undergraduate physics course this is not a homework problem: I'm confused about the underlying...
I have seen many examples of the EOM for a rocket derived for the following cases:
No gravity, No drag
Gravity, No drag
No gravity, linear drag (b*v where b is a constant)
I have never seen
Gravity, linear drag
Gravity, quadratic drag
I took John Taylor's two examples of linear drag and...
Hello All, a few friends of mine and I have devised the ridiculous idea that it would be fun to build a rocket that could do something like the popular weather balloon projects which achieve high altitude for cool visuals (via GoPro or similar). But we want to make it better/faster/cooler...
I was fascinated to learn about dusty plasma fission fragment rockets.
https://en.wikipedia.org/wiki/Fission-fragment_rocket
There's talk that they might enable high delta-V exploration like a manned Jupiter mission! However, they need to be surrounded very many tons of neutron moderator...
I've started making my own sugar-based hobby rocket engines and I want to work on creating a de Laval nozzle for the specific fuel type and configuration I'm using. I don't have the resources to measure things like chamber pressure and exhaust temperature, so I wanted to try and develop an...
Homework Statement
A rocket with initial mass of m0. The engine that can burn gas at a rate defined by m(t)=m0-αt, and expel gas at speed (relative to the rocket) of u(t)=u0-βt. Here, m0, α, u0, and β are all constants. Assume the lift-off from ground is immediate
a) The rocket speed v(t)=...
Homework Statement
In Newtonian mechanics, the rocket equation is derived by solving the simple differential equation -dm U = m dV, where U is the velocity of the expelled material relative to the rocket; a matter of conservation of momentum. In order to get the correct relativistic equation...
Homework Statement
A rocket is fired from from the ground at initial velocity of ##v_0## and at an angle ##\theta##. At its highest height it splits into 2 parts of equal masses. The first part is fired straight up and at velocity ##v_0/2##. Find the angle and intensity of the second part...
Homework Statement
The Saturn V rocket which launched the Apollo space missions had the following specifications: mass at lift-off = 3.0 x 10^6 kg velocity of exhaust gases = 1.0 x 10^4 m/s initial rate of fuel consumption at lift-off = 3.0 x 10^3 kg/s 1.(a) Calculate: (i) the force (thrust)...
By conversation of momentum, the rocket can be propelled forward by ejecting mass like gas.
However, how is the propelling force explained in terms of action and reaction? If gas is ejected, what does the force act on?
I read some time ago a resume of the book the Crack In The Cosmic Egg and this is more or less what it told:
When a rocket acquires light speed its mass becomes infinite which creates a gravity force field that crunches all the universe making it restart.
Its argued that to propel a rocket to...
Homework Statement
A toy rocket engine is securely fastened to a large puck that can glide with negligible friction over a horizontal surface, taken as the xy plane. The 4.00-kg puck has a velocity of 3.00ˆi ms at one instant. Eight seconds later, its velocity is (8.00ˆi + 10.0ˆj) ms. Assuming...