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Juno II
ABMA
Details
Height
24 m
Diameter
2.67 m
GTO
Unknown
LEO
41 kg
Thrust at Liftoff
654 kN
Apogee
Unknown
Launch Cost
Unknown
Maiden Flight
December 6, 1958
Statistics
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Description
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.
Agency
Army Ballistic Missile Agency
ABMA
Links
Wikipedia
en.wikipedia.org