ABOUT JUNO II
Juno II was an American space launch vehicle used during the late 1950s and early 1960s. It was derived from the Jupiter missile, which was used as the first stage.
PAYLOAD CAPACITY
41 kg
TO LEO
90 lbs
LIFTOFF THRUST
654
KILONEWTONS
147,025
POUNDS-FORCE
~877
HORSEPOWER