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Saturn S-IVB

Spacecraft and Launch Vehicles

The S-IVB was the third stage of the Saturn V and the second stage of the Saturn IB launch vehicles. Douglas Aircraft Company built it around a single J-2 rocket engine burning liquid hydrogen with liquid oxygen, and it appears among the products listed for McDonnell Douglas. On lunar missions it fired twice, first to place the spacecraft in Earth orbit after the second stage cut off and then to send it toward the Moon. It evolved from the S-IV stage of the Saturn I. Douglas built two versions, a 200 series for the Saturn IB and a 500 series with a flared interstage for the larger Saturn V, twelve and sixteen flight stages respectively. A surplus tank became the hull of Skylab, the first American space station, and from Apollo 13 onward spent stages were crashed into the Moon to give seismic measurements.

Facts
Year
1966 1
Propulsion
Hydrogen 2
Engine Class
Rocket 2
Mass (kg)
10,000 2
Engine
J-2 2
Connections

Exemplifies

Source S-IVB (Wikipedia)

Of Make

Source McDonnell Douglas (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source McDonnell Douglas (Wikipedia)Products, Missiles and rockets
Quote, Products, Missiles and rockets
Saturn S-IVB third stage

Originated In

Also in Geography Atlas: where this subject originated.

Source McDonnell Douglas (Wikipedia)Lead
Quote, Lead
McDonnell Douglas Corporation was a major American aerospace manufacturing corporation and defense contractor.
Sources
1. NASA: Stages to Saturn: A Technological History of the Apollo/Saturn Launch Vehicles (NASA SP-4206)
NASAPDF page 169, AS-201 launch
Quote, PDF page 169, AS-201 launch
On 26 February 1966, AS-20 1 went through a flawless launch.
View the Source
2. S-IVB (Wikipedia)
  • Lead, engine name
    Built by the Douglas Aircraft Company, it had one J-2 rocket engine.
  • Configuration, propellants
    It carried 252,750 litres (66,770 US gal) of liquid hydrogen (LH2), massing 18,000 kilograms (40,000 lb).
  • Configuration, empty mass
    Empty mass was 10,000 kilograms (22,000 lb)
  • Exemplifies: Orbital Spaceflight, Lead
    The S-IVB (pronounced "S-four-B") was the third stage on the Saturn V and second stage on the Saturn IB launch vehicles.
  • In Group: Orbital Launch Vehicles, Lead, launch vehicle stage
    The S-IVB (pronounced "S-four-B") was the third stage on the Saturn V and second stage on the Saturn IB launch vehicles.
View the Source
McDonnell Douglas (Wikipedia)
  • Products, Missiles and rockets
    Saturn S-IVB third stage
  • Lead
    McDonnell Douglas Corporation was a major American aerospace manufacturing corporation and defense contractor.
View the Source
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