QUOTE (turbonium @ Feb 13 2008, 02:22 AM)

I'd like to go back to this image, with a red arrow pointing to a region that you and Peri claim is "a brightened swath" in the lunar surface, which was caused by the LM descent engine thrust...

Now, I have huge problems with your argument, MID.
Somehow, Turb, I rather expected you would!
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This cannot be a "brightened swath" in the lunar surface caused by the LM DPS engine plume, because it only extends out from the LM on one side, exclusively.
I shall agree that the swath extends to "one side" of the LM. In fact it extends in the direction from which the LM came, and that is generally aft of the LM, possibly a wee bit slanted to one side or another, which is in fact what you see here. Additionally, you see it extend just a little out front...a wee bit.
However, it can only be caused by the LM DPS...but let's wait on that.
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During the LM approach phase,
the altitude decreases from 7000 to 500 feet, the range decreases from approximately 4.5 nautical miles to 2000 feet. The LM trajectory approach angle is
approximately 16° relative to the surface (10.9° nominal to 13.6° maximum).
During the landing phase - from 500 feet altitude down to lunar surface - the LM maintains a trajectory of ~ 16° off the vertical.
http://history.nasa.gov/alsj/nasa58040.pdfTherefore, the DPS engine thrust would also contact the lunar surface at ~ 16° off the vertical, throughout the LM's descent (approach and landing).
This would disrupt (or damage) the lunar surface
all around the region surrounding the LM landing spot. The overall effect would be radial, or slightly elliptical, extending outward, from the LM centerpoint.
The LM would have had to approach the surface at an extreme horizontal trajectory, and have landed on its side, in order to create the one-directional "brightened swath" you say it created in the photo!
I shall commend you on consulting the official documentation describing the descent trajectory phases.
However, you are mis-interpreting what you read, and drawing a rather odd conclusion regarding soil disruption.
First of all, from "High Gate" through "Low Gate" (the places you describe (i.e., ~7000FT through 500FT)) the LM guidance did maintain a 16 degree trajectory relative to the ground. During the Landing Phase, guidance maintained that plane of descent. This Landing Phase trajectory was designed and approved by flight crews because it was a satisfactory plane from which to take manual control of the spacecraft during the terminal landing phase.
You are confusing trajectory of 16 degrees with spacecraft attitude (which equates to the angle of the engine bell to the surface.)
By the time the LM was at around 200 FT, the spacecraft attitude (which was also at 16 degrees pitched up, as-it-were, at Low Gate), the attitude was being pitched flatter so as to be at about 8 degrees. At about 150 FT it was down to 6 degrees.
The computer was nulling horizontal velocity and converting the trajectory to vertical, and it could've landed the vehicle if allowed to. It never was allowed to, and all CDRs took manual control of the terminal phase. Landings all took place essentially vertically, with essentially zero attitude (engine bell flat to the surface), and perhaps a small (1-2 FPS) translational component forward or to one side.
Basically, the LM converted from 16 degrees approach path to almost none, and it's attitude from High Gate went from 16 degrees to essentially zero (meaning, essentially flat, with the crew looking straight out along the surface).
You seem to be interpreting this information as saying the the engine bell was pointing forward 16 degrees all through the landing, which would've caused exhaust to spew forward, ahead of the LM, causing a disruption ahead of the LM by some distance. This was not, and couldn't possibly have been the case. They'd have landed back legs first, and tipped forward onto the surface...not a healthy way to land a LM, and the thrust vector would've been working to push them slightly backwards at that point, which would've made for a really wierd landing...and maybe a catastrophic one...
However, they certainly could've landed with a 16 degree approach path. That's no problem at all in level flight at low velocity. 1 FPS vertical velocity would have a forward translation of 3 FPS at touchdown, for instance, no big deal.
However, it really doesn't matter...because engine exhaust disruption only is caused where the engine exhaust impacts the surface. If you're moving from point A to point B, and the engine exhaust touches the surface along that line, you're going to get disruption along that line, but when the LM stops at point B, that's where the disruption essentially stops, thus, the disruption pattern would logically appear to be off in essentially one direction from the LM, the direction from which it came, primarily, and that is what you see in this photo. There is no physical reason for any uniform disruption out in front of the LM.