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'm returning to grad school for physics this fall, but I've been out of the classroom for thirteen years. (teaching music, of all things) I'm working my way through practice problems for the placement exam, but I don't have any way to verify correct answers for the problems unless I find...
Hello,
I'm trying to build this, but I'm confused a bit about the optimal cheaper way of getting it working, it should be working on 12v battery car and cover 0-90 degree of movement , I've in mind couple of simple ideas, I think I can't build a complicated one like military launch pads...
Homework Statement
A rocket ascends from rest in Earth's gravitational field, by ejecting exhaust with constant speed u. Assume that the rate at which mass is expelled is given by dm/dt = −γm where m is the instantaneous mass of the rocket and γ is a constant; and that the rocket is retarded...
[b]1. a rocket is launched from rest and moves in a straight line at 70degree above the horizontal with an acceleration of 46ms^(-2) . After 30seconds of powered flight , the engines shut off and the rocket follows a parabolic path back to earth. find
1)the maximun altitude reached...
Homework Statement
A rocket ascends from rest in Earth's gravitational field, by ejecting exhaust with constant speed u. Assume that the rate at which mass is expelled is given by dm/dt = −γm where m is the instantaneous mass of the rocket and γ is a constant; and that the rocket is retarded...
Does anybody know how or where I can find a way to figure the Exhaust Temperature of a Rocket. I am considering a problem where I assigned 1.4 atmospheres to the Inlet gas pressure at 300 degrees C.
That it exited into 1 Atmosphere at exit velocity of 325 M per second.
I think that the momentum achieved by a rocket that uses a pressurized ideal gas as it's only propellant, stored in a chamber of fixed volume before being rocketed away. will achieve a final momentum proportional to the Pressure of the gas times the fixed volume of the chamber. momentum ∝...
According to Wikipedia:
http://en.wikipedia.org/wiki/Propulsive_efficiency
the propulsive efficiency of a rocket is at its peak when the rocket is traveling at the same speed as it is ejecting its exhaust. I understand that, but the graph (and equation) on that Wikipedia page (and elsewhere on...
Homework Statement
A toy rocket, launched from the ground, rises
vertically with an acceleration of 23 m/s2 for
11 s until its motor stops.
Disregarding any air resistance, what max-
imum height above the ground will the rocket
achieve? The acceleration of gravity is
9.8 m/s2 .
Answer...
Hi, I'm in first year physics this year and each group in my class has been tasked with making a rocket. Since we're using old pepsi bottles, we just need to make a nose cone, tail fins, and perhaps a little paper on the main body to draw a design on it.
I looked a little bit online, but I...
I've been posing this question to physicist folk for 10 years, mySpace 6 years ago, and here (don't know when, when I had an older account), and I see that others bring it up on occasion. I will refine it to meet current objections.
You have a photonic drive spaceship. It has a (classical) mass...
I'm hoping that someone can guide me toward some literature on 'rocket science'. I know that is not very descriptive, but essentially, I would like to learn about the engineering and physics principles that govern rocket flight (to include propulsion and guidance). I have found some books...
Homework Statement
A rocket of initial mass of 2.85x10^6 kg is on the surface of the earth. if the initial acceleration is .20g, what is the required thrust? if the fuel is burned at a rate of 14,500 kg/s, with what speed is it ejected from the rocket?
Homework Equations
The...
In the Tsiolkovsky rocket equation derivation there is a part that says:
\frac{dV}{dt} = -\upsilon_e \frac{1}{m} \frac{dm}{dt}
"Assuming v_e, is constant, this may be integrated to yield:"
\Delta V\ = v_e \ln \frac {m_0} {m_1}
How does this work? The differential is an operator...
Homework Statement
A rocket, initially at rest on the ground, accelerates straight upward from rest with constant acceleration 34.3 m/s^2. The acceleration period lasts for time 10.0 s until the fuel is exhausted. After that, the rocket is in free fall.
Find the maximum height y_max...
Can someone provide me to a guide, book or some kind of tutorial that would help me in learning how to simulate the flow of gases in a rocket nozzle?
I am trying to investigate the effect of my expansion ratios, nozzle geometry and other design parameters and simulate it.
I would be very...
Me and a few friends are having a contest to see who can create a rocket that has the longest hangtime when shot out by air pressure built up in a container. I thought about doing a parachute, but that's risky considering that it could slow down the rocket when it is ascending and it might not...
Homework Statement
This is not exactly a homework question. Special relativity question.
See attach. 1.
Two spaceships are passing each other, having their fronts marked F and F'. When F' sees the other's rear passing the front of F', F' fires a rocket. Clearly it misses, since the F SS is...
Rocket design --300km range, 5-15kg payload, 200mg accuracy
Hi, I'm working on a project for a mech engineering class where we have to design a remote control vehicle to carry a small payload 300km. It must be able to survive rain, crosswind speeds up to 70km/h, temperatures up to 50 degree...
The Problem:
A 4.60 kg rocket is launched directly upward from Earth at 9.00 km/s
What altitude above the Earth's surface does the rocket reach?
Relevant Equations:
v = √ (2GM/r)
The Attempt:
m = 4.60 kg
v = 9km/s = 9000m/s
G = 6.67 x 10^-11
9000^2 = 2(6.67^-11)(4.60)/r...
Homework Statement
In a two-stage rocket, the exhaust velocity for the first stage burn is 3000 m/s and for the second stage burn is 3000 m/s. Assume that during the entire sequence of burns the rocket is still near enough to the surface of the Earth to approximate the external gravitational...
A rocket of mass m=1.20x10^3 kg is launched vertically upward from the Earth's surface with an initial speed v0 = 7.00 km/s.
Calculate the maximum height H of point A above the Earth's surface at which the rocket will momentarily come to rest, before it starts falling back on the earth.
So I...
Homework Statement
Two powerless rockets are on a collision course. The rockets are moving with speed v = 0.800c (rocket 1) and v = -.600c (rocket 2) and are initially 2.52 * 10^12m apart as measured by Liz, an Earth observer. Both rockets are 50m long as measured by Liz.
a) What are their...
I did a bottle rocket yesterday (2 liter bottle). I made 4 fins and the end of the fins touch the ground instead of the bottle's opening. I also equip my rocket with a parachute (hide under the nose cone). In addition, I added a modeling clay to my nosecone too! When I tested it, my teacher said...
Homework Statement
Say I've got a rocket payload (there's no thrust, it's just dead weight) falling to Earth from an altitude of 260km and I want to calculate the time it takes it to fall to 160km. It's far enough away from Earth that I can't make the assumption that gravity is constant (it...
Homework Statement
An engine supplies an upward force of 9.00N to an initially stationary toy rocket, of mass 54.0g, for a distance of 25.0m. The rocket rises to a height of 339 meters before falling back to the ground. What was the magnitude of the average force of air resistance on the...
Could a "pure-electric" laser-propelled space rocket be mere decades away?
I know that there probably isn't a battery capable of making this practical yet, but if it were possible to store energy at a high enough density, wouldn't that make it theoretically possible to make a rocket that uses...
Homework Statement
A physics student launches a model rocket from the ground at t=0. The rocket ascends with a constant vertical acceleration of a1= 2.5m/s^2 until T1= 5.0s, when the acceleration increases to a2= 5.0m/s^2 until T2= 10.0s. When t>T2, the engine shuts down entirely.
(b) What is...
Question I) For a single stage rocket: T = 955.23 kN, n = 16, Isp = 400 s and m0 = 70, 000 kg. The rocket is launched into a vertical trajectory. Neglecting drag and assuming g is constant at its sea level value, Find (a) the time until burnout, (b) burnout altitude, (c) burnout velocity, (d)...
Homework Statement
A 10.2 kg weather rocket generates a thrust of 177.0 N. The rocket, pointing upward, is clamped to the top of a vertical spring. The bottom of the spring, whose spring constant is 385.0 N/m, is anchored to the ground. Initially, before the engine is ignited, the rocket sits...
I'm trying to solve a rocket problem and have found no clear answer on how to do this. If I have a rocket in space (no significant gravitational forces, no drag, etc.) with a known constant thrust (T), mass flow rate (mdot), exhaust velocity (Ve), total initial mass including propellant (Mi)...
Hello, I'm trying to solve the rocket equation in a nonuniform gravitational field. The standard rocket equation at a distance x from the center of a planet of mass M gives:
m*d^2x/dt^2 + v_e*dm/dt = -GmM/x^2
where v_e is the relative exhaust velocity.
Multiplying by dx/dt and assuming...
I've written a program to show the trajectory of a rocket around the Earth with initial conditions that can be manipulated to fix a circular or elliptical orbit.
We start with Newton's 2nd law and use the equation a=F/m in freespace (so m can divide out) to get a 2nd order ODE and solve by...
Homework Statement
A rocket at rest in space, where there is virtually no gravitational force, has a mass of 2.55 * 105 kg, of which 1.81*105 kg is fuel.The engine consumes fuel at the rate of 480 kg/s and the xhaust speed is 3.27 m/s. The engine is fired for 250 s.
Find the thrust of the...
Homework Statement
A rocket for use in deep space is to have the capability of boosting a pay load ( plus the rocket frame and engine) of 3 metric tonnes to an achieved speed of 10000m/s with an engine and fuel designed to produce an exhaust velocity of 2000m/s.
a) How much fuel and...
Homework Statement
Suppose that the acceleration of a model rocket is proportional to the difference between 100 ft/sec and the rocket's velocity. If it is initially at rest and its initial acceleration is 50 ft/sec2, how long will it take to accelerate to 80 ft/s?
The Attempt at a...
I'm looking for a small camera to use in my rocket. It's about a 7' rocket, 4" diameter and 3" long viewing window. I've heard that the choices are either cmos or ccd but I don't know the difference between the two. I'm only looking to spend up to $100 (really looking in the $50 range). Any...
Homework Statement
Hi, i have constructed a rocket car out of a meccano kit and used a 2l water bottle filled with 200ml of water and pressured gas as a means to propel it forwards. The distance that it has to travel is 16.5m
I am having difficulty calculating the energy stored in the...
Hi all! I've just finished writing a program in python that determines the position of a rocket in the Earth moon system. Initially it is in circular orbit around the Earth and then it is given a velocity boost at some point in it's orbit to make it travel to the moon.
I started all 3 bodies...
Homework Statement
A spacecraft begins a journey with rest mass Mi. Its method of propulsion involves converting matter entirely to photons, which are emitted in the direction opposite to the direction of motion. After a period of acceleration the rest mass has been reduced to Mf. Show...
Homework Statement
Suppose that during the launch of a rocket from the surface of the earth, an astronaut onboard the rocket stands on a bathroom scale and measures her weight to be 3.6 times her normal weight. Determine the acceleration of the rocket. Homework Equations
Fnet \sumF = ma
or...
Homework Statement
rockwt has reliability of 0.81 for the first trail. if the manned rocket fails there is probability of 0.05 of a catastrophic explosion in which case the abort system can not be used. id the abort can be attempted the system has a reliability of 0.90
find 1- the...
Ok, so I've come with this idea with my cousin to make a bottle rocket, but I'm really being beaten up by this idea. I've tried to search for a lot of tutorials, but none of them really made my mind.
I have everything in mind but the "ignitor" (which releases the pressure). Most tutorials...
"A rule of thumb is that for every ten-percent increase in efficiency for rocket fuel, the payload of the rocket can double.”
Can someone assist me with a simple formula to model this rule-of-thumb?
What happens to the payload if the rocket fuel efficiency increases twenty to thirty percent?
Homework Statement
Hello, I am currently a gr 12 high school student, and I am stuck in a problem. Please help :)
The problem: Consider the motion of a rocket near the surface of the Earth. In this case, mass, in the form of gas is expelled from the rocket to propel the rocket upwards. A...
A 20 000kg rocket exhausts gases at a constant 600kg per second at 300ms^-1
a) Calculate the momentum of the exhaust gases
b) Deduce the thrust applied to the rocket engines
Any help would be much appreciated
Normally, one would think that an object generating large amounts of thrust would fly all over the place with no clear direction. How does a rocket stabilize and launch perfectly straight up?
Homework Statement
A rocket is launched at an angle of 58.0° above the horizontal with an initial speed of 98 m/s. It moves for 3.00 s along its initial line of motion with an acceleration of 28.0 m/s2. At this time its engines fail and the rocket proceeds to move as a free body.
Maximum...
So I'm looking and researching to build a small liquid-fueled rocket engine. So far I think my choice for fuel is definitely unleaded gasoline because of it's high impulse when mixed with Gas-state O2 and how easy it is to obtain.
Previously, I was looking at using Hydrogen Peroxide (H202) for...
Homework Statement
My rocket was angled at 79 degrees from the vertical,
I calculated its maximum vertical height to be 60 meters,
The total flight time was 7 seconds
Experimental horiz distance is 40 yds (should be 36.6 meters)
Homework Equations
This is part of my problem, I am...