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Specifications
- Status
- retired
- Height
- 24 m
- Diameter
- 2.67 m
- Mass
- 55,000 kg
- Stages
- 4
- Thrust
- 654 kN
- Payload to LEO
- 41 kg
- First flight
- 1958-12-06
- Total launches
- 10
- Success / Fail
- 5 / 5
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.
Payloads it launched
5 loaded