Variable-mass system

Rockets, which lose significant amounts of mass as fuel during flight, are an example of a variable-mass system.

In mechanics, a variable-mass system is a collection of matter whose mass varies with time. It can be confusing to try to apply Newton's second law of motion directly to such a system.[1][2] Instead, the time dependence of the mass m can be calculated by rearranging Newton's second law and adding a term to account for the momentum carried by mass entering or leaving the system. The general equation of variable-mass motion is written as

where Fext is the net external force on the body, vrel is the relative velocity of the escaping or incoming mass with respect to the center of mass of the body, and v is the velocity of the body.[3] In astrodynamics, which deals with the mechanics of rockets, the term vrel is often called the effective exhaust velocity and denoted ve.[4]

  1. ^ Kleppner, D.; Kolenkow, R. J. (1978) [1973]. An Introduction to Mechanics. London: McGraw-Hill. pp. 133–139. ISBN 0-07-035048-5.
  2. ^ Basavaraju, G; Ghosh, Dipin (1985-02-01). Mechanics and Thermodynamics. Tata McGraw-Hill. pp. 162–165. ISBN 978-0-07-451537-2.
  3. ^ Plastino, Angel R.; Muzzio, Juan C. (1992). "On the use and abuse of Newton's second law for variable mass problems". Celestial Mechanics and Dynamical Astronomy. 53 (3). Netherlands: Kluwer Academic Publishers: 227–232. Bibcode:1992CeMDA..53..227P. doi:10.1007/BF00052611. ISSN 0923-2958. S2CID 122212239. Retrieved 2011-12-30.
  4. ^ Benson, Tom. "Ideal Rocket Equation". NASA. Archived from the original on 11 October 2007. Retrieved 30 December 2011.

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