V 2 Rocket Diagram. Write down the coordinates of b and c. The practical limit for v e is about 2510 3 ms for conventional non nuclear hot gas propulsion systems.
A rockets acceleration depends on three major factors consistent with the equation for acceleration of a rocket. The variables include acceleration a time t displacement d final velocity vf and initial velocity vi. The rocket has two stages.
Learners can modify the propulsion force the resistance forces friction and air resistance and the mass of the rocket sled.
S ic measured 42 m 138 feet tall and 10 m 33 feet in diameter and had a dry weight of 131 metric tons 289000. The atlas v is an expendable medium lift launch system and member of the atlas rocket family. The practical limit for v e is about 2510 3 ms for conventional non nuclear hot gas propulsion systems. 1 injector assembly 2 o ring 3 liquid fuel 4 gaseous oxygen 5 engine mount 6 coolant 7 fuel spray nozzle 8 combustion chamber 9 outer shell 10 coolant.