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Second Stage for SA-9
 

 

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Summary

Description
English: The second Stage for a Saturn I rocket. (SA-9)

Orginal relase to the photo:

The Saturn I S-IV stage (second stage) assembly for the SA-9 mission underwent the weight and balance test in the hanger building at Cape Canaveral. The S-IV stage had six RL-10 engines which used liquid hydrogen and liquid oxygen as its propellants arranged in a circle. Each RL-10 engine produced a thrust of 15,000 pounds, a total combined thrust of 90,000 pounds. The SA-9 mission was the first Saturn with operational payload Pegasus I, meteoroid detection satellite, and launched on February 16, 1965.
Deutsch: Die zweite Stufe einer Saturn I (SA-9).
Date 1 November 1964(1964-11-01)
Source https://mix.msfc.nasa.gov/abstracts.php?p=1506 direct link to the picture:https://mix.msfc.nasa.gov/IMAGES/HIGH/6416600.jpg
Author unknown
Permission
(Reusing this file)

https://mix.msfc.nasa.gov/copyright.html

Licensing

Public domain This file is in the public domain because it was created by NASA. NASA copyright policy states that "NASA material is not protected by copyright unless noted". (See Template:PD-USGov, NASA copyright policy page or JPL Image Use Policy.)

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Photo's description:
The second Stage for a Saturn I rocket. (SA-9) Orginal relase to the photo: The Saturn I S-IV stage (second stage) assembly for the SA-9 mission underwent the weight and balance test in the hanger building at Cape Canaveral. The S-IV stage had six RL-10 engines which used liquid hydrogen and liquid oxygen as its propellants arranged in a circle. Each RL-10 engine produced a thrust of 15,000 pounds, a total combined thrust of 90,000 pounds. The SA-9 mission was the first Saturn with operational payload Pegasus I, meteoroid detection satellite, and launched on February 16, 1965.
Licensing:
Public Domain


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