none 

Statements about this table:
the parameter that have a third phase of 0.50 m be the diameter
the second stage that have the third phase of 20kn be 73kn
the third stage that have the first phase of 5443 kg be 63 kg
the parameter that have a third phase of 20kn be thrust
the parameter that have a 3rd stage of 0.50 m be the length
the third stage that have a 1st stage of 5443 kg be 126 kg
parameter
1st stage
2nd stage
3rd stage
4th stage
gross mass
54431 kg
462 kg
126 kg
42 kg
empty mass
5443 kg
231 kg
63 kg
21 kg
thrust
667kn
73kn
20kn
7kn
isp
248 s (2.43kn路s / kg)
214 s (2.10kn路s / kg)
214 s (2.10kn路s / kg)
214 s (2.10kn路s / kg)
burn time
182 s
6 s
6 s
6 s
parameter
1st stage
2nd stage
3rd stage
4th stage
length
18.28 m
1.0 m
1.0 m
1.0 m
diameter
2.67 m
1.0 m
0.50 m
0.30 m
engine :
rocketdyne s - 3d
eleven sergents
three sergents
one sergent
propellant
lox / rp - 1
solid fuel
solid fuel
solid fuel