SOME APPROACHES CONCERNING THE DETERMINATION OF THE VELOCITY OF A ROCKET INTO INTERPLANETARY SPACE
This paper presents a method of calculation for a fundamental parameter of the missile flight dynamics, movement speed in a fluid medium. It is used in this sense of angular momentum theorem and momentum theorem in fluid mechanics.
Keywords: rocket, reaction force, mass forces, trajectory, mass flow, volume control, non-inertial reference system, exhaust nozzle
Cuvinte cheie: rachetă, forţă de reacţie, forţe masice, traiectorie de zbor, debit masic, volum de control, sistem de referinţă neinerţial, ajutaj de evacuare