MCT - Google Sheets

	A	B	C	D
1	ITS SSTO Calculator
2	dV for Ascent	9300	m/s	Velocity change to be executed, normally between 9km/s and 10km/s for LEO
3	dV for Landing	0	m/s	Velocity change to be executed, normally between 500m/s and 1000m/s for landing
4	Isp	352	s	Average specific impulse for rocket engines
5	Propellant mass	1100	t	Total mass of useful propellant
6	Dry mass	85	t	Dry mass of spacecraft including unused propellant, engines and structure
7	Extra Propellant	Yes		Whether extra useful propellant can be added up to the 380t limit for cargo
8	Payload Return	No		Whether or not to return the payload to the surface of the Earth
9	# RaptorVac	0		Number of Vacuum Raptor Engines
10	# RaptorSL	6		Number of Sea-Level Raptor Engines
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13	Payload mass	-5.16901465	1.947043643
14	Non return	-5.16901465	1.947043643
15	Payload mass	1.947043643	t	Mass of payload
16	Liftoff Mass	1565	t	Total liftoff mass
17	Liftoff Thrust	11400	kN	Thrust of all Sea-Level Engines
18	Liftoff TWR	0.7425428183		Thrust-to-Weight Ratio
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