Earth Land | Earth Insert | Earth Inject | Mars Launch | Mars Land | Mars Insert | Mars Inject | Abort Reserve | Stage 2 Ascent | Booster Landing | Boost Back | Earth Launch | Units | |
---|---|---|---|---|---|---|---|---|---|---|---|---|---|
Starting Mass | tonnes | ||||||||||||
Ending Mass | tonnes | ||||||||||||
Burned Mass | tonnes | ||||||||||||
Propellant Availiable | tonnes | ||||||||||||
Oxydizer Capacity | tonnes | ||||||||||||
Fuel Capacity | tonnes | ||||||||||||
Propellant Volume | cubic meters | ||||||||||||
Oxydizer Volume | cubic meters | ||||||||||||
Fuel Volume | cubic meters | ||||||||||||
Tank Material | square meters | ||||||||||||
Tank Mass | tonnes | ||||||||||||
Start TWR | ratio | ||||||||||||
End TWR | ratio | ||||||||||||
Engines Required | engines | ||||||||||||
Engine Count | engines | ||||||||||||
Engine Mass | kg | ||||||||||||
Engine Thrust | kN |