Juno II Vehicle Overview
A complete overview of the Juno II launch vehicle, including launch stats, vehicle info and launch locations.
Basic Info
Name
Juno II
Family
Juno
Manufacturer
First Launch
6 Dec 1958
Successful Launches
5
Failed Launches
5
Rocket Info
Status
Inactive
Stages
3-4
Length
24 m
Diameter
2.67 m
Launch Mass
55 tons
Thrust
654 kN
Reusability
Not Reusable
Payload Info
LEO Capacity
41 kg
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.
Launch Sites used by Juno II
Cape Canaveral Space Force Station
Historic U.S. military rocket launch site, pivotal in space exploration and national security.
📍 FL, United States
🚀 987 Launches