ASTE 520 HW 20 Flashcards
1
Q
Time to burnout (for a rocket with constant propellant mass flow rate)
A
2
Q
Tsiolkovsky Rocket Equation
A
3
Q
Integrated Form of The Rocket Equation (without gravity -(1/2)g_e*t_b^2 term)
A
4
Q
Integration By Parts Formula
A
5
Q
Common Integrals - Integral of log(x) or ln(x)
A
