Advertisement

Abstract

  • To introduce the elements of rocket propulsion useful in flight dynamic modeling.

  • To model the velocity impulse of single- and multi-stage rockets.

  • To discuss the optimal selection of stage payload ratios of multi-stage rockets with examples.

Keywords

Rocket Engine Launch Vehicle Geosynchronous Orbit Velocity Impulse Rocket Propulsion 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

Preview

Unable to display preview. Download preview PDF.

Unable to display preview. Download preview PDF.

Copyright information

© Birkhäuser Boston 2007

Personalised recommendations