This is the second, or S-II-F/D, or Facilities Checkout/Dynamic Test Stage, of the Saturn V launch vehicle. This stage of the rocket was not meant to fly but was used for ground tests pior to the actual flight tests. As in the flyable version of the Saturn V, the stage shown here is fitted with five J-2 rocket engines, all inoperable. The Dynamic Test version of the rocket was extremely important in Apollo program - it proved the validity of the vehicle's structural design. In its flyable form, the 363-foot long, 33-foot diameter operational version of the Saturn V rocket took a dozen astronauts toward the Moon during 1969-1972 and is considered one of the greatest engineering achievements in history. The second stage was transferred by NASA to the Smithsonian in 1975.
Display Status
This object is not on display at the National Air and Space Museum. It is either on loan or in storage.
Object Details
Country of Origin
United States of America
Type
CRAFT-Missile & Rocket Parts
Manufacturer
Rockwell International Corporation
Dimensions
Length, total, from J-2 engine nozzle to Handling Structure, 87 feet; length, from nozzle to rim before Handling Strucure, 79 feet; length, Handling Structure, 8 feet; diameter, rocket body, 33 feet
Materials
Skin, central section, a plastic honeycomb; corrugated sections around base, after J-2 engines, and around top of body, before Temporary Handling Structure, aluminum; stainless steel and other steels in J-2 engines; Temporary Handling Structure, steel.
Inventory Number
A19750676000
Credit Line
Transferred from NASA
Data Source
National Air and Space Museum
Restrictions & Rights
Usage conditions apply
For more information, visit the Smithsonians Terms of Use.