Using a propellant of molecular weight 15 and flame temperature 3300 K, determine the rocket throat and exhaust areas required for a thrust of 500 kN and an ideal specific impulse of 300 sec. The ambient pressure is 0.1 MPa, and the specific-heat ratio of the propellant is 1.4. How much thrust would this rocket

2. Celsius..Farenheit..Kelvin

1. Measurements is process of measuring or size of something

3. Ampere is measure of the amount of electric charge per unit time

4. Electric current is the rate of flow of charge.

5. Luminous intensity: is a quantity for characterizing a light source.

6. Mole: unit of measurement for amount of substance in SI system

7. Plane angle we simply say that angle in two dimensions

Where as solid angle is in three dimensions