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Propellant mass fraction information


In aerospace engineering, the propellant mass fraction is the portion of a vehicle's mass which does not reach the destination, usually used as a measure of the vehicle's performance. In other words, the propellant mass fraction is the ratio between the propellant mass and the initial mass of the vehicle. In a spacecraft, the destination is usually an orbit, while for aircraft it is their landing location. A higher mass fraction represents less weight in a design. Another related measure is the payload fraction, which is the fraction of initial weight that is payload. It can be applied to a vehicle, a stage of a vehicle or to a rocket propulsion system.

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Propellant mass fraction

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In aerospace engineering, the propellant mass fraction is the portion of a vehicle's mass which does not reach the destination, usually used as a measure...

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Payload fraction

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mass and the total vehicle mass at the start of its journey. It is a function of specific impulse, propellant mass fraction and the structural coefficient...

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Mass fraction

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Fuel mass fraction Propellant mass fraction (aerospace), the amount of mass left behind such as the stages of rockets Payload fraction (aerospace), the...

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Mass ratio

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for mass fraction are always less than 1. Rocket fuel Propellant mass fraction Payload fraction Zubrin, Robert (1999). Entering Space: Creating a Spacefaring...

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Tsiolkovsky rocket equation

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performance. In other words, the propellant mass fraction is the ratio between the propellant mass and the initial mass of the vehicle. In a spacecraft...

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Propellant

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A propellant (or propellent) is a mass that is expelled or expanded in such a way as to create a thrust or another motive force in accordance with Newton's...

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Balloon tank

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its shape. Balloon tanks are very light, and this permits a good propellant mass fraction. A disadvantage of balloon tanks is that if pressurization fails...

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Aerospace engineering

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Engineering and efficiency Preflight engineering Mass ratio Payload fraction Propellant mass fraction Tsiolkovsky rocket equation Efficiency measures Gravity...

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Apsis

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and in 2000 it was about 282.895°; by 2010, this had advanced by a small fraction of a degree to about 283.067°, i.e. a mean increase of 62" per year. For...

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Ammonium perchlorate composite propellant

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perchlorate composite propellant (APCP) is a solid rocket propellant. It differs from many traditional solid rocket propellants such as black powder or...

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Oberth effect

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propellants it carries. In terms of the energies involved, the Oberth effect is more effective at higher speeds because at high speed the propellant has...

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Antimatter rocket

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its "wet" mass ( M 0 {\displaystyle M_{0}} )(with propellant mass fraction) to "dry" mass ( M 1 {\displaystyle M_{1}} )(with payload) fraction ( M 0 M 1...

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Liquid rocket propellant

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The highest specific impulse chemical rockets use liquid propellants (liquid-propellant rockets). They can consist of a single chemical (a monopropellant)...

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Orbital period

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is the orbit's semi-major axis G is the gravitational constant, M is the mass of the more massive body. For all ellipses with a given semi-major axis the...

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Orbital decay

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incineration by the star's radiation (such as for comets). Collisions of stellar-mass objects are usually accompanied by effects such as gamma-ray bursts and detectable...

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Orbital eccentricity

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energy (total energy divided by the reduced mass), μ the standard gravitational parameter based on the total mass, and h the specific relative angular momentum...

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Lagrange point

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{M_{2}}{M_{1}+M_{2}}}} is the mass fraction of M2 and x = r R {\displaystyle x={\frac {r}{R}}} is the normalised distance. If the mass of the smaller object (M2)...

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Hohmann transfer orbit

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thrust rather than the short applications of high thrust. The amount of propellant mass used measures the efficiency of the maneuver plus the hardware employed...

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Gravity assist

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the speed of the spacecraft. However, rocket thrust takes propellant, propellant has mass, and even a small change in velocity (known as Δv, or "delta-v"...

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Escape velocity

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leaving the Solar System Newton's cannonball Oberth effect – burning propellant deep in a gravity field gives higher change in kinetic energy Two-body...

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Orbital speed

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other bodies of the system combined, its speed relative to the center of mass of the most massive body. The term can be used to refer to either the mean...

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Orbital propellant depot

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propellant to a transfer stage headed to the Moon, Mars, or possibly a geosynchronous orbit. Since all or a fraction of the transfer stage propellant...

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Mass driver

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excessively increase propellant mass needed under the rocket equation, with too high a fraction of energy going into accelerating propellant not used yet. Higher...

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