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Nose Cones
Ogive Nose
Conical Nose
Blunt Nose
Payload
Payload Fairing
Payload Bay
Tanks
Fuel Tank (S)
Fuel Tank (M)
Fuel Tank (L)
Engines
Merlin-class
Rutherford-class
Solid Booster
Stability
Left Fin
Right Fin
Grid
100%
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↑ from Parts Library on the left
Assembly Status
○ NO-GO
incomplete
TWR
—
Total Mass
0.0 t
Δv
275 m/s
Burn Time
—
○
Nose Cone
○
Engine
○
Fuel Tank
○
Fins
Override
Payload (kg)
Fuel (kg)
Dry Mass (kg)
Thrust (kN)
Diameter (m)
Propellant
LOX/RP-1
LOX/LH2
UDMH/N2O4
Solid
Nose Cone
Ogive
Conical
Blunt
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