I've been browsing the "
Saturn V Flight Manual" published in 1969 which the forward
describes as "This manual is prepared to provide the astronaut with a single source
reference to the characteristics and functions of the SA-507 launch vehicle".
Imagine being handed the manual to this baby.
And you thought the warnings in the owners manual for the Husqvarna chain-saw
you bought were scary.
How about stuff like this on page 3-9 of the Saturn V owner's manual which you
have to recollect at liftoff whilst you are pulling 6 G's -
Quote:
With S-IC/S-II staging, the S-II SEP light will illuminate.
The light will go out approximately 30 seconds later when the interstage structure
is jettisoned. A severe overheating problem will occur if the structure is not
jettisoned at the nominal time. Under the worst conditions, abort limits will
be reached within 25 seconds from nominal jettison time. Confirmation from Mission
Control of interstage failure to jettison serves as the second abort cue.
During the earth orbit phase of the mission the S-II SEP light is again used.
It is turned ON to indicate the beginning of restart preparations at T6 + 0.1 seconds.
It is turned OFF at T6 + 41.5 seconds to indicate O2H2 burner ignition. It is
turned ON again at T6 + 8 minutes 40 seconds and OFF again at at T6 + 9 minutes
+ 20 seconds to indicate translunar injection (TLI) commit (engine start - 10 seconds).
WARNING
After TLI commit (T6 + 9 minutes 20 seconds) the only way remaining to effect a
TLI inhibit is with the T-handle.
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Wow. Love it!
Paying attention? Because we will be asking questions after the lecture.
The manual here -
http://www.ibiblio.org/apollo/Docume...nual-SA507.pdf