"The significance of parameters affecting the heat transfer to the liquid hydrogen in the Saturn S-IVB stage for the lunar orbit rendezvous mission."
The Saturn S-IVB stage has a requirement for orbiting around the earth for up to 4.5 hours with approximately 60 percent of its initial propellant remaining at the end of the coast (prior to restart) . Extensive analyses must be performed to insure that this requirement is met. Both the maximum and...
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| Format: | Electronic |
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University of Alabama in Huntsville Archives
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| Online Access: | http://libarchstor2.uah.edu/digitalcollections/items/show/10397 |