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Saturn A-2

Index Saturn A-2

Studied with the Saturn A-1 in 1959, the Saturn A-2 was deemed more powerful than the Saturn I rocket, consisting of a first stage, which actually flew on the Saturn IB, a second stage which contains four S-3 engines that flew on the Jupiter IRBM and a Centaur high-energy liquid-fueled third stage. [1]

5 relations: Centaur (rocket stage), PGM-19 Jupiter, Saturn A-1, Saturn I, Saturn IB.

Centaur (rocket stage)

Centaur has been designed to be the upper stage of space launch vehicles and is used on the Atlas V. Centaur was the world's first high-energy upper stage, burning liquid hydrogen (LH2) and liquid oxygen (LOX).

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PGM-19 Jupiter

The PGM-19 Jupiter was the first nuclear tipped, medium-range ballistic missile (MRBM) of the United States Air Force (USAF).

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Saturn A-1

Saturn A-1, studied in 1959, was projected to be the first version of Saturn I and was to be used if necessary before the S-IV liquid hydrogen second stage became available.

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Saturn I

The Saturn I (pronounced "Saturn one") was the United States' first heavy-lift dedicated space launcher, a rocket designed specifically to launch large payloads into low Earth orbit.

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Saturn IB

The Saturn IB (pronounced "one B", also known as the Uprated Saturn I) was an American launch vehicle commissioned by the National Aeronautics and Space Administration (NASA) for the Apollo program.

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References

[1] https://en.wikipedia.org/wiki/Saturn_A-2

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