data
1x 30MW Nuclear generator
6x Nuclear thermal rocket / liquid annular reactor system
each LARS' Mass-20t
thrust 350t
Exhaust Velocity-12.5kmps
length-170m
Propellant tank h=60m
d=13m
each 3kt of CH4
dry mass-1.5kt
wet mass-42kt
mass ratio-28
ΔV=41.6kmps
unmanned