the maximum velocity of a rocket is approximated by:
Delta_V = go*ISP*ln(Mi/Mf)
where Delta_V = the change in velocity
go = 32.2 ft/22
ISP = the specific impulse
Mi = initial mass
Mf = final mass
mp = propellant mass
mo = stage inert mass
mf = stage total mass
This equation has to be solved for each stage considering the masses of all of the fallowing stages and payloads
Stage 1
mo (lb) 300000
mp (lb) 4492000
mf (lb) 4792000
Mi (lb) 6200600
Mf (lb) 1708600
ISP 263
delta V 10915.79
Stage 2
mo (lb) 95000
mp (lb) 942000
mf (lb) 1037000
Mi (lb) 1408600
Mf (lb) 466600
ISP 421
delta V 14977.96
Stage 3 mo (lb) 34000
mp (lb) 228000
mf (lb) 262000
Mi (lb) 371600
Mf (lb)143600
ISP 421
delta V 12889.05
payload mass (lb) 109600
Max Speed ft/s 38782.80
Max Speed Mph 26442.82
In short, ignoring aerodynamic friction and assuming a constant gravitation acceleration the maximum achievable velocity is about ~26500 mph
120mph stock
In an Apollo capsule sitting on top of a Saturn V rocket.
110mph
110mph
saturn v did not land the moon but was the luna module
Vehicle speed sensor is located on top of the differential on the transmission. Access is from under the car
It was the fifth rocket in the Saturn-class, named after the planet Saturn, or the Mythological god Saturn.
A 2004-2007 cadillac cts-v will do a 0-60 in 4.6 seconds and has a top speed of 163. A 2009 cts-v will do 0-60 in 3.9 seconds and has a top speed 193 mph.
85 mph
I top mine at 190 km\h with the 2.2L 4 cyl and a 5 speed transmission. It would go faster but it is electronically locked.
Saturn ION 2.2 L ecotec engine has a top speed of 78.6 mph which is fairly fast.
No part of the Saturn V rocket was reusable.