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The 'spinning' of the CSM is more to do with temperature control than maintaining an accurate trajectory.
There is no heat from the Sun outside of Earths armosphere, and they have never proven that there is. The 'slow cooker' thing is rubbish.
originally posted by: GaryN
a reply to: onebigmonkey
The 'spinning' of the CSM is more to do with temperature control than maintaining an accurate trajectory.
That was denied by NASA, and it is in the mission reports.
The rotation was to stabilise the the craft in order to keep the antenna for the navigation and guidance computer pointing towards Earth, so they didn't loose contact and become lost. One of the crew had had to remain awake at all times to ensure the antenna was lined up, but with the rotation they found they could all sleep at the same time and not loose contact.
There is no heat from the Sun outside of Earths armosphere, and they have never proven that there is. The 'slow cooker' thing is rubbish.
All attitude control functions were satisfactorily performed throughout
the mission. The passive thermal control roll maneuver was used during
translunar and transearth coast.
The digital autopilot was used to initiate the passive thermal control
mode at a positive roll rate of 0.3 deg/sec, with the positive longitudinal
axis of the spacecraft pointed toward the ecliptic north pole
during translunar coast (the ecliptic south pole was the direction used
during transearth coast). After the roll rate was established, thruster
firing was prevented by turning off all 16 switches for the service module
thrusters. In general, this method was highly successful in that it
maintained a satisfactory spacecraft attitude for very long periods of
time and allowed the crew to sleep without fear of either entering gimbal
lock or encountering unacceptable thermal conditions.
originally posted by: GaryN
a reply to: onebigmonkey
There is no heat from the Sun outside of Earths armosphere, and they have never proven that there is. The 'slow cooker' thing is rubbish.
They would have been weightless until they fired the decent engine. Here's a little discussion about the Thrust-to-weight indicator they had on the instrument panel in front of the LMP. www.hq.nasa.gov...
Just before the eingine was shutdown, T/W (in multiple of lunar gravity) would have been about 3.6 - or about 0.6 earth gravities.