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Orbital mechanics and Rocket

Shortcuts: Differences, Similarities, Jaccard Similarity Coefficient, References.

Difference between Orbital mechanics and Rocket

Orbital mechanics vs. Rocket

Orbital mechanics or astrodynamics is the application of ballistics and celestial mechanics to the practical problems concerning the motion of rockets and other spacecraft. A rocket (from Italian rocchetto "bobbin") is a missile, spacecraft, aircraft or other vehicle that obtains thrust from a rocket engine.

Similarities between Orbital mechanics and Rocket

Orbital mechanics and Rocket have 19 things in common (in Unionpedia): Aerodynamics, Aerospace engineering, Ballistics, Conservation of energy, Delta-v, Drag (physics), Escape velocity, Force, Gravity, Kinetic energy, Mass ratio, Newton's laws of motion, Orbit, Parabola, Potential energy, Spacecraft, Spacecraft propulsion, Specific orbital energy, Tsiolkovsky rocket equation.

Aerodynamics

Aerodynamics, from Greek ἀήρ aer (air) + δυναμική (dynamics), is the study of the motion of air, particularly its interaction with a solid object, such as an airplane wing.

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Aerospace engineering

Aerospace engineering is the primary field of engineering concerned with the development of aircraft and spacecraft.

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Ballistics

Ballistics is the field of mechanics that deals with the launching, flight, behavior, and effects of projectiles, especially bullets, unguided bombs, rockets, or the like; the science or art of designing and accelerating projectiles so as to achieve a desired performance.

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Conservation of energy

In physics, the law of conservation of energy states that the total energy of an isolated system remains constant, it is said to be ''conserved'' over time.

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Delta-v

Delta-v (literally "change in velocity"), symbolised as ∆v and pronounced delta-vee, as used in spacecraft flight dynamics, is a measure of the impulse that is needed to perform a maneuver such as launch from, or landing on a planet or moon, or in-space orbital maneuver.

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Drag (physics)

In fluid dynamics, drag (sometimes called air resistance, a type of friction, or fluid resistance, another type of friction or fluid friction) is a force acting opposite to the relative motion of any object moving with respect to a surrounding fluid.

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Escape velocity

In physics, escape velocity is the minimum speed needed for an object to escape from the gravitational influence of a massive body.

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Force

In physics, a force is any interaction that, when unopposed, will change the motion of an object.

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Gravity

Gravity, or gravitation, is a natural phenomenon by which all things with mass or energy—including planets, stars, galaxies, and even light—are brought toward (or gravitate toward) one another.

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Kinetic energy

In physics, the kinetic energy of an object is the energy that it possesses due to its motion.

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Mass ratio

In aerospace engineering, mass ratio is a measure of the efficiency of a rocket.

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Newton's laws of motion

Newton's laws of motion are three physical laws that, together, laid the foundation for classical mechanics.

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Orbit

In physics, an orbit is the gravitationally curved trajectory of an object, such as the trajectory of a planet around a star or a natural satellite around a planet.

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Parabola

In mathematics, a parabola is a plane curve which is mirror-symmetrical and is approximately U-shaped.

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Potential energy

In physics, potential energy is the energy possessed by an object because of its position relative to other objects, stresses within itself, its electric charge, or other factors.

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Spacecraft

A spacecraft is a vehicle or machine designed to fly in outer space.

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Spacecraft propulsion

Spacecraft propulsion is any method used to accelerate spacecraft and artificial satellites.

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Specific orbital energy

In the gravitational two-body problem, the specific orbital energy \epsilon\,\! (or vis-viva energy) of two orbiting bodies is the constant sum of their mutual potential energy (\epsilon_p\,\!) and their total kinetic energy (\epsilon_k\,\!), divided by the reduced mass.

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Tsiolkovsky rocket equation

The Tsiolkovsky rocket equation, classical rocket equation, or ideal rocket equation, describes the motion of vehicles that follow the basic principle of a rocket: a device that can apply acceleration to itself using thrust by expelling part of its mass with high velocity and thereby move due to the conservation of momentum.

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The list above answers the following questions

Orbital mechanics and Rocket Comparison

Orbital mechanics has 114 relations, while Rocket has 258. As they have in common 19, the Jaccard index is 5.11% = 19 / (114 + 258).

References

This article shows the relationship between Orbital mechanics and Rocket. To access each article from which the information was extracted, please visit:

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