ROCKET EQUATION

	A	B	C	D	E	F	G	N
1
2			Metric		Convenient			https://en.wikipedia.org/wiki/Tsiolkovsky_rocket_equation
3		DeltaV	2,259	m/s	2.26	km/s
4	Exhaust Velocity	Ve	3,700	m/s	3.70	km/s
5	Specific Impulse	Isp	380	s			https://en.wikipedia.org/wiki/SpaceX_Starship
6	Standard Gravity	g0	9.81	m/s/s			https://en.wikipedia.org/wiki/Standard_gravity
7	Initial Mass	m0	1,750,750	kg	1,750.75	tons
8	Final Mass	m1	950,750	kg	950.75	tons	Burns half of standard tank leaving higher final mass
9
10	Fuel		1,500,000		1,500.00	tons
11	half fuel		750,000		750.00	tons
12
13
14			Metric		Convenient
15		DeltaV	8,013	m/s	8.01	km/s
16	Exhaust Velocity	Ve	3,700	m/s	3.70	km/s
17	Specific Impulse	Isp	380	s			https://en.wikipedia.org/wiki/SpaceX_Starship
18	Standard Gravity	g0	9.81	m/s/s			https://en.wikipedia.org/wiki/Standard_gravity
19	Initial Mass	m0	1,750,750	kg	1,750.75	tons
20	Final Mass	m1	200,750	kg	200.75	tons
21
22	Fuel		1,550,000	tons	1,550.00	tons
23	half fuel		775,000	tons	775.00	tons
24
25
26
27	Total	DeltaV	10,272	km/s
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