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Originally posted by intrptr
reply to post by Saint Exupery
Thank you for that most in depth and informative reply. You helped me answer an old mystery and I will clarify my spelling mistake about "helo carrying a helo" up front. It was too late to go back and edit. I meant a helo, I was told a Chinook, carrying a "standby capsule" suspended beneath it to drop in case of reentry failure. Ok, that is the heresy part told second hand to me in my youth.
Originally posted by Saint Exupery
I'd like to know how it was reported at the time.
Originally posted by intrptr
Just like I saw and you say.
My memory about when they saw the chute is that that appeared on screen just after the "we read you" from the capsule. Then the response was almost immediate. "we see you on the mains" and massive cheering in the control room. The screen in the control room showed the capsule suspended from chutes. Did they hold back cheering till then to be sure? Dunno.
Did anyone test those depleted batteries or measure signal strength...
or explain how the manual corridor adjustment to reentry glide slope was made with such precision, before firing of explosive bolt(s) to jettison LEM prior to reentry?
Originally posted by intrptr
reply to post by Saint Exupery
At this point, the Apollo capsule was generating aerodynamic lift (it really was an honest-to-god "flying saucer" - even if it was only gliding) and Command Module Pilot (CMP) Jack Swigert was flying it towards the recovery target area.
Wait. What? He was flying it after reentry and prior to chute deployment? How could he know where they were? And what on the capsule provided aerodynamic control? You lost me there.
The baseline descent rolls the entry module in a way that offsets its center of mass to create a small lift force. This keeps the shallowly descending vehicle higher in thinner air, limiting the deceleration forces to 3 to 4 g's. The maneuver also helps steer the path toward a desired landing region.
If the normal shallow descent isn't possible, the autopilot performs what is called a ballistic, or nonlifting, entry, falling more quickly into thicker air and consequently enduring as much as twice the peak deceleration.
Originally posted by r2d246
Here's a simple question...
Independent researches have reviewed the camera used on the first [mission] to the moon.
It has NO SPECIAL PROTECTION measures what so ever.
That means the film would be subject to endless radiation,
heat from the sun as high as 200 degrees and cold.
How would the film stay in tact (sic).
And how would they come back with such exact picture perfect images...
...considering they had very little experience taking pictures...
...and the clumbsy apperatus that didn't allow for easy picture taking.
I don't see this being reasonable...
...even if they did somehow make it there.
Originally posted by intrptr
post by Saint Exupery
At this point, the Apollo capsule was generating aerodynamic lift (it really was an honest-to-god "flying saucer" - even if it was only gliding) and Command Module Pilot (CMP) Jack Swigert was flying it towards the recovery target area.
Wait. What? He was flying it after reentry and prior to chute deployment? How could he know where they were? And what on the capsule provided aerodynamic control? You lost me there.
As the Earth's atmosphere was entered aerodynamic forces created torques that were determined by the CM's shape and centre of mass location. In the correct attitude these torques were in the direction of a stable trim orientation with the heat shield forward and flight path nearly parallel to one edge of the conical CM surface.The guidance system commanded the reaction jets to dampen out oscillations about this trim orientation. The resulting angle of attack of the entry shape caused an aerodynamic lift force which was used to control the entry path by rolling the CM about the wind axis under control of the guidance system. Range control was achieved by rolling such that a part of the aerodynamic lift was either "up or down". Across-range control was achieved by choosing which side the horizontal lift component was to be on. The maneuver footprint was 2870 miles by 345 miles.The early part of the entry phase is concerned with safely reducing the high velocity by dissipating the energy effects of the drag forces. At lower velocity ,later in the entry descent, the guidance system was more concerned with controlling the descent to achieve the desired landing (splashdown) area.
Let me ask you this. How would they even take a dump on the moon? There's no outhouse and no leaves to wipe. so you're saying they held it in the whole time?
Originally posted by mikellmikell
I always liked the questions about why all the photographs are perfect.Well in the days before digital probably 2/3 of a professionals pictures were trash at least mine were. Nowdays I bet it's more like 80% perhaps 90% have no value so you don't show them to anybody