APPLIED PROJECT:
ROCKET SCIENCE.
ERIDA ZELA.
IDA KAPEDANI.
KLEJDINA SINO.
MELINA CERVANAKU.
04
PROBLEM.
BACKGROUND RECAP.
In this project, we want to minimize the total mass of a 3-stage rocket engine given:
•Final velocity vf
•Structural factor S
•Exhaust speed c
•Payload mass A
Problem 4: Expression for Minimum Mass as Function of vf.
05
PROBLEM.
Problem 5: Getting into Low Earth Orbit
06
PROBLEM.
Problem 6: Deep Space Launch with Final Velocity = 24,700 mi/h
05 AND 06
PROBLEM.