Faster access than browser!Similarities between Rocket and Spacecraft propulsion
Rocket and Spacecraft propulsion have 43 things in common (in Unionpedia): Acceleration, Airbreathing jet engine, Attitude control, De Laval nozzle, Delta-v, Drag (physics), Escape velocity, Force, G-force, Gravitational acceleration, Gravity drag, Heat engine, Hybrid-propellant rocket, Internal combustion engine, Konstantin Tsiolkovsky, Liquid-propellant rocket, List of rocket launch sites, Lists of rockets, Low Earth orbit, Momentum, Multistage rocket, Newton's laws of motion, Non-rocket spacelaunch, Nozzle, Nuclear thermal rocket, Orbit, Parachute, Reaction engine, Reaction wheel, Robert H. Goddard, ..., Rocket engine, Rocket engine nozzle, Rocket launch, Satellite, Solar thermal rocket, Solid-propellant rocket, Space probe, Spacecraft, Specific impulse, Thrust, Tripropellant rocket, Tsiolkovsky rocket equation, Velocity. Expand index (13 more) »
Acceleration
In physics, acceleration is the rate of change of velocity of an object with respect to time.
Acceleration and Rocket · Acceleration and Spacecraft propulsion ·
Airbreathing jet engine
An airbreathing jet engine (or ducted jet engine) is a jet engine propelled by a jet of hot exhaust gases formed from heated and expanded air that is drawn into the engine via a compressor, typically a centrifugal or axial type.
Airbreathing jet engine and Rocket · Airbreathing jet engine and Spacecraft propulsion ·
Attitude control
Attitude control is controlling the orientation of an object with respect to an inertial frame of reference or another entity like the celestial sphere, certain fields, and nearby objects, etc.
Attitude control and Rocket · Attitude control and Spacecraft propulsion ·
De Laval nozzle
A de Laval nozzle (or convergent-divergent nozzle, CD nozzle or con-di nozzle) is a tube that is pinched in the middle, making a carefully balanced, asymmetric hourglass shape.
De Laval nozzle and Rocket · De Laval nozzle and Spacecraft propulsion ·
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.
Delta-v and Rocket · Delta-v and Spacecraft propulsion ·
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.
Drag (physics) and Rocket · Drag (physics) and Spacecraft propulsion ·
Escape velocity
In physics, escape velocity is the minimum speed needed for an object to escape from the gravitational influence of a massive body.
Escape velocity and Rocket · Escape velocity and Spacecraft propulsion ·
Force
In physics, a force is any interaction that, when unopposed, will change the motion of an object.
Force and Rocket · Force and Spacecraft propulsion ·
G-force
The gravitational force, or more commonly, g-force, is a measurement of the type of acceleration that causes a perception of weight.
G-force and Rocket · G-force and Spacecraft propulsion ·
Gravitational acceleration
In physics, gravitational acceleration is the acceleration on an object caused by the force of gravitation.
Gravitational acceleration and Rocket · Gravitational acceleration and Spacecraft propulsion ·
Gravity drag
In astrodynamics and rocketry, gravity drag (or gravity losses) is a measure of the loss in the net performance of a rocket while it is thrusting in a gravitational field.
Gravity drag and Rocket · Gravity drag and Spacecraft propulsion ·
Heat engine
In thermodynamics, a heat engine is a system that converts heat or thermal energy—and chemical energy—to mechanical energy, which can then be used to do mechanical work.
Heat engine and Rocket · Heat engine and Spacecraft propulsion ·
Hybrid-propellant rocket
A hybrid-propellant rocket is a rocket with a rocket motor which uses rocket propellants in two different phases.
Hybrid-propellant rocket and Rocket · Hybrid-propellant rocket and Spacecraft propulsion ·
Internal combustion engine
An internal combustion engine (ICE) is a heat engine where the combustion of a fuel occurs with an oxidizer (usually air) in a combustion chamber that is an integral part of the working fluid flow circuit.
Internal combustion engine and Rocket · Internal combustion engine and Spacecraft propulsion ·
Konstantin Tsiolkovsky
Konstantin Eduardovich Tsiolkovsky (a; Konstanty Ciołkowski; 19 September 1935) was a Russian and Soviet rocket scientist and pioneer of the astronautic theory of ethnic Polish descent.
Konstantin Tsiolkovsky and Rocket · Konstantin Tsiolkovsky and Spacecraft propulsion ·
Liquid-propellant rocket
A liquid-propellant rocket or liquid rocket is a rocket engine that uses liquid propellants.
Liquid-propellant rocket and Rocket · Liquid-propellant rocket and Spacecraft propulsion ·
List of rocket launch sites
This article constitutes a list of rocket launch sites.
List of rocket launch sites and Rocket · List of rocket launch sites and Spacecraft propulsion ·
Lists of rockets
There are several different types of rockets.
Lists of rockets and Rocket · Lists of rockets and Spacecraft propulsion ·
Low Earth orbit
A low Earth orbit (LEO) is an orbit around Earth with an altitude of or less, and with an orbital period of between about 84 and 127 minutes.
Low Earth orbit and Rocket · Low Earth orbit and Spacecraft propulsion ·
Momentum
In Newtonian mechanics, linear momentum, translational momentum, or simply momentum (pl. momenta) is the product of the mass and velocity of an object.
Momentum and Rocket · Momentum and Spacecraft propulsion ·
Multistage rocket
A multistage rocket, or step rocket is a launch vehicle that uses two or more rocket stages, each of which contains its own engines and propellant.
Multistage rocket and Rocket · Multistage rocket and Spacecraft propulsion ·
Newton's laws of motion
Newton's laws of motion are three physical laws that, together, laid the foundation for classical mechanics.
Newton's laws of motion and Rocket · Newton's laws of motion and Spacecraft propulsion ·
Non-rocket spacelaunch
Non-rocket spacelaunch refers to concepts for launch into space where some or all of the needed speed and altitude are provided by something other than rockets, or by other than expendable rockets.
Non-rocket spacelaunch and Rocket · Non-rocket spacelaunch and Spacecraft propulsion ·
Nozzle
A nozzle is a device designed to control the direction or characteristics of a fluid flow (especially to increase velocity) as it exits (or enters) an enclosed chamber or pipe.
Nozzle and Rocket · Nozzle and Spacecraft propulsion ·
Nuclear thermal rocket
A nuclear thermal rocket is a proposed spacecraft propulsion technology.
Nuclear thermal rocket and Rocket · Nuclear thermal rocket and Spacecraft propulsion ·
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.
Orbit and Rocket · Orbit and Spacecraft propulsion ·
Parachute
A parachute is a device used to slow the motion of an object through an atmosphere by creating drag (or in the case of ram-air parachutes, aerodynamic lift).
Parachute and Rocket · Parachute and Spacecraft propulsion ·
Reaction engine
A reaction engine is an engine or motor that produces thrust by expelling reaction mass, in accordance with Newton's third law of motion.
Reaction engine and Rocket · Reaction engine and Spacecraft propulsion ·
Reaction wheel
A reaction wheel (RW) is a type of flywheel used primarily by spacecraft for three axis attitude control, which doesn't require rockets or external applicators of torque.
Reaction wheel and Rocket · Reaction wheel and Spacecraft propulsion ·
Robert H. Goddard
Robert Hutchings Goddard (October 5, 1882 – August 10, 1945) was an American engineer, professor, physicist, and inventor who is credited with creating and building the world's first liquid-fueled rocket.
Robert H. Goddard and Rocket · Robert H. Goddard and Spacecraft propulsion ·
Rocket engine
A rocket engine uses stored rocket propellant mass for forming its high-speed propulsive jet.
Rocket and Rocket engine · Rocket engine and Spacecraft propulsion ·
Rocket engine nozzle
A rocket engine nozzle is a propelling nozzle (usually of the de Laval type) used in a rocket engine to expand and accelerate the combustion gases produced by burning propellants so that the exhaust gases exit the nozzle at hypersonic velocities.
Rocket and Rocket engine nozzle · Rocket engine nozzle and Spacecraft propulsion ·
Rocket launch
A rocket launch is the takeoff phase of the flight of a rocket.
Rocket and Rocket launch · Rocket launch and Spacecraft propulsion ·
Satellite
In the context of spaceflight, a satellite is an artificial object which has been intentionally placed into orbit.
Rocket and Satellite · Satellite and Spacecraft propulsion ·
Solar thermal rocket
A solar thermal rocket is a theoretical spacecraft propulsion system that would make use of solar power to directly heat reaction mass, and therefore would not require an electrical generator, like most other forms of solar-powered propulsion do.
Rocket and Solar thermal rocket · Solar thermal rocket and Spacecraft propulsion ·
Solid-propellant rocket
A solid-propellant rocket or solid rocket is a rocket with a rocket engine that uses solid propellants (fuel/oxidizer).
Rocket and Solid-propellant rocket · Solid-propellant rocket and Spacecraft propulsion ·
Space probe
A space probe is a robotic spacecraft that does not orbit the Earth, but, instead, explores further into outer space.
Rocket and Space probe · Space probe and Spacecraft propulsion ·
Spacecraft
A spacecraft is a vehicle or machine designed to fly in outer space.
Rocket and Spacecraft · Spacecraft and Spacecraft propulsion ·
Specific impulse
Specific impulse (usually abbreviated Isp) is a measure of how effectively a rocket uses propellant or jet engine uses fuel.
Rocket and Specific impulse · Spacecraft propulsion and Specific impulse ·
Thrust
Thrust is a reaction force described quantitatively by Newton's third law.
Rocket and Thrust · Spacecraft propulsion and Thrust ·
Tripropellant rocket
A tripropellant rocket is a rocket that uses three propellants, as opposed to the more common bipropellant rocket or monopropellant rocket designs, which use two or one propellants, respectively.
Rocket and Tripropellant rocket · Spacecraft propulsion and Tripropellant rocket ·
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.
Rocket and Tsiolkovsky rocket equation · Spacecraft propulsion and Tsiolkovsky rocket equation ·
Velocity
The velocity of an object is the rate of change of its position with respect to a frame of reference, and is a function of time.
The list above answers the following questions
- What Rocket and Spacecraft propulsion have in common
- What are the similarities between Rocket and Spacecraft propulsion
Rocket and Spacecraft propulsion Comparison
Rocket has 258 relations, while Spacecraft propulsion has 207. As they have in common 43, the Jaccard index is 9.25% = 43 / (258 + 207).
References
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