Soldato
- Joined
- 7 Aug 2004
- Posts
- 11,302
As title, I have been looking around and it seems once in orbit, the Apollo stack had about 30000kg of fuel to get to the moon, land and back again.
But I was thinking A)
1) How much fuel does Titan II use to get to the moon
2) How much LESS fuel would it need if it was a completely solid rocket motor perfectly built to fire the correct burn at various stages to lunar orbit.
ONLY orbit the moon and come back, not land on the moon.
But I was thinking A)
1) How much fuel does Titan II use to get to the moon
2) How much LESS fuel would it need if it was a completely solid rocket motor perfectly built to fire the correct burn at various stages to lunar orbit.
ONLY orbit the moon and come back, not land on the moon.