LVOHV shipping costs

	B	C	D	M	N	O	P
1
2				Delta-V
3				Delta-V
4				From "Human Lunar Exploration Architectures", NASA-JPL, John Connolly (2012)
5
6				FROM	TO	DV (m/s)
7				LEO	TLI	3000
8				TLI	LLO	970
9				LLO	Luna	1870
10				LLO	Earth	1310
11
12
13				https://space.stackexchange.com/questions/23992/why-is-a-near-rectilinear-halo-orbit-proposed-for-lop-g-formerly-known-as-deep
14				LEO	NRHO	3428,5
15				NRHO	Earth	411,5
16
17				http://i.imgur.com/WGOy3qT.png
18				Luna	LEO	2850	w/ Aerobraking
19				Luna	LEO	5660	w/o Aerobraking
20				LEO	TMI	3600
21				TMI	LMO	2150	w/o Aerobraking
22	Hydrolox Vacuum Starship-like			TMI	LMO	750	w/ Aerobraking
23	Hydrolox Vacuum Starship-like			LMO	Mars	500	w/ Aerobraking + propulsive landing
24	Cost per launch	30	[M$]	Mars	LMO	3600
25	MAX PL to LEO	250	[s-1]	LMO	TEI	2100
26	MAX mass propellant	1100	[t]	TEI	LEO	400	w/ Aerobraking
27	m_s	130	[t]	TEI	LEO	3600	w/o Aerobraking
28	Isp	440	[s-1]	TEI	LLO	1300
29	mixture ratio	6	[/]	LLO	TMI	1300
30				LEO	GEO	3910
31				GEO	Earth	1500	with aerobraking
32				Luna	GEO	4000	with aerobraking
33				GEO	TLI	2150
34
35				Luna	HMO	2400
36
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39				Luna	EML1	2360
40				EML1	TMI	1060
41				TEI	EML1	1060
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