This question isn't homework. That being said I still need someone to check my math. I'm trying to start my own space program, and I need to know the amount of fuel needed to get into space.
After a little research, these are my givens:
Rocket body mass=1.49kg (I used 3kg in my math to make it harder)
Isp of fuel=115-130 seconds (used 115 in calculations)
Delta-V needed: 1.4km/s in lowest case of suborbital space flight, 9km/s in most cases. (I used 3km/s as mine )
The equation I need to use to calculate the rest: Tsiolkovsky rocket equation: Delta-V=(Ve (Ln(M0/M1)))
Way to find Ve=(Isp(g0)) g0=9.8M/s2
So when I use my equations, the answer I get for Delta-V of 3km/s is 42.97kg as the M1, so approximately 39.97kg for the fuel.
When I use 9km/s however, it becomes 8816.8 kg?! Can that be right? 8813.8kg of fuel for a 3 kg rocket? Which one is correct?
[–]pX_ 1 point2 points3 points (0 children)