SOLID ROCKET WITH A MOTOR THAT USES FUEL

DEVICE USED TO IGNITE(START) MATERIALS

ROUND SPOT AT END OF PIPE USED TO CONTROL JETOF GAS OR LIQUID

AERODYNAMIC LADING EDGE OF A ROCKET

PART OF ROCKET THAT CONTROLS STABILITY AND CONTROLS DIRECTION

RESPONSES TO INPUTS AND OUPUTS

POINT AT WHICH ALL OF THE MASS OF AN OBJECT CAN THOUGHT TO BE CONCENTR

SINGLE POINT AT WHICH ALL AERODYNAMIC FORCES ARE CONCENTRATED

RATIO OF ONE SUBSTANCE OUT OF TOTAL IN ROCKET