Space · launch vehicle
Juno II
ABMA
RETIRED
At a glance
Launches
10
Success rate
50%
5 ok · 5 failed
Payload to LEO
41 kg
Payload to GTO
—
Manufacturer
Army Ballistic Missile AgencyStatus
RetiredFirst flight
06 Dec 1958Reusable
NoHeight
24 mDiameter
2.67 mLaunch mass
55 tLiftoff thrust
654 kNStages
4Launch cost
—Booster landings
—Links
WikipediaAbout
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.
Source The Space Devs — Launch Library 2
Last checked 29 Sept 2026