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Equations of Motion of a Rocket

by Nasa Technical Reports Server (Ntrs)
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Current price ₹1,339.00
Original price ₹1,446.00
Original price ₹1,446.00
Original price ₹1,446.00
(-7%)
₹1,339.00
Current price ₹1,339.00

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Book cover type: Paperback
  • ISBN13: 9781287246961
  • Binding: Paperback
  • Subject: N/A
  • Publisher: Bibliogov
  • Publisher Imprint: Bibliogov
  • Publication Date:
  • Pages: 26
  • Original Price: USD 14.75
  • Language: English
  • Edition: N/A
  • Item Weight: 68 grams
  • BISAC Subject(s): General

In considering the motion of the rocket, at each instant of time only the state of those material particles which a t that instant are within the control surface passing through the exterior surface of the body of the rocket and the exit section of the nozzle shall be included. In order t o obtain the equations of motion of the rocket, the following procedure is used. An arbitrary but fixed instant of time is considered. A fictitious solid body is denoted by S with mass m, which would be obtained if the rocket at the instant t solidified and ceased giving off particles. The solid body S will not be homogeneous; in some of its parts, it will have the density of a metal and in other parts the density of a gas, and so forth. It shall be assumed that the fictitious solid body S is invariably fixed to the body of the rocket and from the instant t onwards (instant of solidification) moves together with the rocket. The momentum of the body S shall be denoted by Q.

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