Abstract A generalized rocket formula is derived from a first principles approach. The resulting expression of the thrust is applied to advanced space propulsion systems and a possible link between the asymptotic propellant velocity and the velocity at thruster exit is given. An estimation of the thrust modification due to spacecraft–plume interactions is also considered.
A generalization of the rocket formula and its application to advanced space propulsion systems
Acta Astronautica ; 68 , 1-2 ; 34-38
2010-07-26
5 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
A generalization of the rocket formula and its application to advanced space propulsion systems
Online Contents | 2011
|NTRS | 1993
|NTIS | 1993
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