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Apollo trivia questions
Just a few things I was thinking about:
1) Was there any footage of staging from the vantage point of Stage 1 of the Saturn V? We've all seen it from the vantage point of Stage 2. Similarly, is there footage the staging from S-IV, since we've all seen it from Stage II (or was it S-IB?). 2) During capsule re-entry, did the CM enter the atmosphere going in the direction of earth rotation or against it? I heard the Apollo re-entries were quit a bit quicker and more stressful than shuttle entries, and I though part of the reason may have been that earth-orbiting ships would have to re-enter in the direction of rotation, while the Apollos would not necessarily have that restriction. |
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wrote:
Just a few things I was thinking about: 1) Was there any footage of staging from the vantage point of Stage 1 of the Saturn V? We've all seen it from the vantage point of Stage 2. Similarly, is there footage the staging from S-IV, since we've all seen it from Stage II (or was it S-IB?). See http://www.thebest.net/jduncan/cookcam/cookcam.htm There was no footage of the staging from the S-IVB because it entered orbit and the camera could not be recovered |
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In article .com,
wrote: 1) Was there any footage of staging from the vantage point of Stage 1 of the Saturn V? We've all seen it from the vantage point of Stage 2. Hmm, not sure. I know it was done for the Saturn I and IB, but I've never seen a complete list of the Saturn V camera pods. 2) During capsule re-entry, did the CM enter the atmosphere going in the direction of earth rotation or against it? Generally more or less with the rotation, but this wasn't a big issue. The main reason the Apollo reentries were unusually hard and hot was that they were coming in from deep space, moving about 40% faster than an orbital spacecraft and hence hitting the atmosphere harder. Relative to that, the difference between reentering with and against the rotation, while not entirely insignificant, wasn't large. I heard the Apollo re-entries were quit a bit quicker and more stressful than shuttle entries... There were also technological reasons for that. A capsule, like the Apollo CM, can't generate as much lift as a winged vehicle like the shuttle orbiter. (It can generate *some*, by flying tilted, and Apollo did that.) So it descends more quickly into thicker air, and decelerates more quickly and gets hotter in the process. On the other hand, its ablative heatshield, which burns and boils off during reentry, can briefly handle much harsher conditions than the shuttle's tiles can, so a short sharp reentry works well for it. -- "Think outside the box -- the box isn't our friend." | Henry Spencer -- George Herbert | |
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Paolo Ulivi wrote: wrote: Just a few things I was thinking about: 1) Was there any footage of staging from the vantage point of Stage 1 of the Saturn V? We've all seen it from the vantage point of Stage 2. Similarly, is there footage the staging from S-IV, since we've all seen it from Stage II (or was it S-IB?). See http://www.thebest.net/jduncan/cookcam/cookcam.htm There was no footage of the staging from the S-IVB because it entered orbit and the camera could not be recovered Dead link. |
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"Paolo Ulivi" wrote in message ... wrote: Just a few things I was thinking about: 1) Was there any footage of staging from the vantage point of Stage 1 of the Saturn V? We've all seen it from the vantage point of Stage 2. Similarly, is there footage the staging from S-IV, since we've all seen it from Stage II (or was it S-IB?). See http://www.thebest.net/jduncan/cookcam/cookcam.htm There was no footage of the staging from the S-IVB because it entered orbit and the camera could not be recovered That doesn't really answer his question though since the 1st stage obviously did NOT enter orbit. (and in any case, the film pods were to my knowledge separated from the boosters and reentered separately.) |
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