Game in the Brain

 The Saturn-V is a great sample rocket. 

Its performance and Stats are readily available and its a great baseline since we want our performance to be compared against this Iconic rocket. 

Things that is not in Wikipedia are the following:

1. The Total Volume is 414 Dtons or as big as a Fat Trader except that 90% is Propulsion instead of the 10-20% of a Fat Trader is Fuel. 

1. 	S-IC first stage	S-II second stage	S-IVB third stage	TOTAL
   HEIGHT	42.0 m	24.9 m	17.9 m
   Diameter	10.0 m	10.0 m	6.6 m
   Volume	3,298.7 m^3	1,953.3 m^3	611.0 m^3	5,252.0 kg
   Dtons	233.1 DTON	138.0 DTON	43.2 DTON	371.2 DTON
   Dry Weight	131,000.0 kg	36,000.0 kg	10,000.0 kg	167,000.0 kg
   Total Wt	2,300,000.0 kg	480,000.0 kg	119,000.0 kg	2,780,000.0 kg
   FULL LOAD	2,780,000.0 kg	599,000.0 kg	119,000.0 kg
   Engines	Rocketdyne F-1	Rocketdyne J-2	Rocketdyne J-2
   Number	5	5	1

2. As a Baseline I start modifying the % of propulsion at a given TL. 
2.  the Acceleration which we can get is 1.3Gs
1. 
   

   Thrust (N)	35,100,000 N	4,900,000 N	1,033,100.0 N
   Accel (m/s^2)	12.63	8.18	8.68
   Accel (G)	1.29	0.83	0.89
   Propulsion	2,169,000.0 kg	444,000.0 kg	109,000.0 kg
   Kg/s	12,910.7 kg	1,156.3 kg	741.5 kg
   Dtons/S	0.912	0.082	0.052
   Burn/Accel(Dton/G)	0.71	0.10	0.06

2. I like how the rocket hovering Illustrated a 1G thrust vs 1G effect = Hovering. 

3. The Context of how its not the Performance of the Rockets that Improved over time but the Reliability. Their Thrust to Mass Ratio was roughly to 70-80. Comparing the 196B  Shuttle Program 1.4B per launched (135 launches, 2 failures and partial failures) vs  49B Apollo Program with 4.7B per Launch.