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  Apollo lunar module touchdown dynamics (Page 2)

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Author Topic:   Apollo lunar module touchdown dynamics
nasamad
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posted 01-03-2015 03:47 PM     Click Here to See the Profile for nasamad   Click Here to Email nasamad     Edit/Delete Message   Reply w/Quote
Looking at the images of the engine bell, I'd say the gap between it and the lunar surface is only about 1 inch in places (judging this in relation to the 10 inch skirt extension) and this is after the skirt buckled.

Also given the location of the LRV deployment hardware in the photographs and the perceived angle and direction of the buckling, this would tally up with the audio of the landing where Irwin is calling "minus 1" to Scott in the final few seconds before touchdown. I believe he is reading the speed in feet per second from the cross pointer that the LM is travelling backwards.

LM-12
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posted 01-03-2015 04:16 PM     Click Here to See the Profile for LM-12     Edit/Delete Message   Reply w/Quote
It is my understanding that "minus 1" was the descent rate in feet per second, and that the LM was translating to the right of forward at touchdown.

If you haven't seen this already, the ALSJ has an enhanced (light adjusted) version of engine bell photo AS15-88-11882.

nasamad
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posted 01-04-2015 12:16 PM     Click Here to See the Profile for nasamad   Click Here to Email nasamad     Edit/Delete Message   Reply w/Quote
Your absolutely right, my mistake. I just read the mission report and it does state a forward and right direction at landing. I read the minus one in the transcript and audio and thought Irwin was giving Scott rates of drift once they were within a few feet of the surface but it is descent rate.

Strangely it does state that the +Y and +Z footpads were the first to touch the surface, then the other two. I wonder of the engine bell may have touched when the LM rocked back into the crater?

LM-12
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posted 01-04-2015 12:40 PM     Click Here to See the Profile for LM-12     Edit/Delete Message   Reply w/Quote
One thing the CDR definitely did not want to do was to have the LM going backwards at touchdown.

Blackarrow
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posted 01-04-2015 06:06 PM     Click Here to See the Profile for Blackarrow     Edit/Delete Message   Reply w/Quote
quote:
Originally posted by Blackarrow:
I specifically disagree with the comment quoted...
To recap, the issue is whether damage to the Apollo 15 lunar module's engine bell was caused by contact with the lunar surface or engine-exhaust back-pressure.

At the outset, I should declare an interest: I wrote the Apollo 15 chapter in "Footprints in the Dust" and in October, 2008 when I interviewed Dave Scott, I discussed this very issue with him. During the interview and in follow-up emails he agreed that the damage was probably caused by the engine bell impacting the rim of a small crater which had been completely obscured by dust during the final descent.

I am confident that this is the correct conclusion, and that it is supported by (at least) 2 Apollo commanders and a MIT engineering professor.

Strange as it may seem, Apollo 16 is the starting point to understand this issue. When John Young and Charlie Duke were on the surface, Duke is reported in the ALSJ at 119:17:36 as saying: "...the engine bell is about 6 inches off the ground and it's not crushed at all."

There are no Apollo 16 photographs showing close-up views of the underside of "Orion" but a decent enlargement of part of AS16-107-17434 shows the engine bell clear of the surface. I estimated about 4-5 inches, but I will not quibble with Duke's figure of 6 inches: he was there. However, the key point is that "Orion" is resting on flat ground, and in spite of that, the clearance under the engine bell is barely the gap between thumb-tip and forefinger-tip when stretched apart.

Young and Duke both noted with some concern that "Orion" was only 10 feet from a fairly steep-sided crater. In the "Apollo 16 Technical Crew Debriefing" John Young said (page 9.17): "If the rear strut had been over that hole, we'd have been just like the Apollo 15 guys. We would have been landing on the first 3 and the engine bed."

I suggest in the context, the word "bed" is a typo and he actually said "bell" but either way it is clear what he is saying.

Referring back to the Apollo 16 photograph, consider the effect on the clearance between the engine bell and the ground if "Orion's" rear legs had been in a crater or a depression leaving "Orion" tilted 11 degrees from the horizontal (as in the case of "Falcon.")

Returning now to Apollo 15, on inspecting the exterior of "Falcon", Scott reported (at 119:57:14): "Tell the Program Manager [Jim McDivitt] I guess I got his engine bell. It's a little rise right under the centre of the LM. The rear leg's in a crater and the rim of the crater is right underneath the engine bell."

In the "Apollo 15 Technical Crew Debriefing" (at p. 10.3) both Scott and Irwin agreed that the front landing pad was, at most, only lightly in contact with the ground. The landing pad actually pivotted round when Irwin stepped on it.

During my 2008 interview with Dave Scott I asked whether it was possible that "Falcon" was actually resting on three legs and the engine bell. He agreed that this was probable. In a long follow-up email after the interview (which actually includes the long quote from the Apollo 15 Mission Report which LM-12 quoted in his 2nd January post) Scott wrote:

Your comment about the engine bell being in contact with the surface, yet the front footpad was 'loose' seems to indicate that we may have made contact with the bell at about the same time as the footpads, hence a 5-point landing. If so, the LM struts would not have absorbed as much of the impact as designed, and maybe that's why the 'bump.'
This is an important point: the landing-legs were designed to absorb much of the landing forces, but contact between the engine bell and the ground would have transmitted impact forces directly through the structure of the LM, explaining the jarring landing which rattled everything in the LM cabin.

Let's now turn to the photographic record. Kipp Teague provided the ALSJ with an enhanced image taken by Scott of the underside of "Falcon." The Apollo 15 Mission report refers to the engine bell damage as "buckling." I am not an engineer, but I must suggest that the visible damage looks entirely consistent with a direct impact with the rising ground under the LM. It crumples inward, and does not seem consistent with an internal pressure build-up caused by reflected exhaust gas.

I accept that the closest part of the bell may be an inch or two off the surface, but it definitely appears to me that the rest of the bell is imbedded into the rising crater wall. Furthermore, the large white object, apparently the "jettison bag" is resting on the ground beside the engine bell. This provides scale, and strongly suggests that the part of the bell beyond the bag is in contact with the ground.

I said I am not an engineer, but David Mindell is. The author of "Digital Apollo", Mindell is Professor of Engineering Systems at M.I.T. At page 255 of his book, discussing the jarring impact, he writes:

"Indeed, there had been a bump: the LM was overlapping the edge of a small crater, with the bell of the descent engine dropping directly on its rim, buckling it."

In conclusion, I suggest that when careful consideration is given to the very limited engine bell clearance on flat ground, it is almost impossible to see how contact between the ground and the engine bell could be avoided if the rear of the LM drops into a crater, leaving the LM 11 degrees off the horizontal (as alluded to by John Young). I'm sure a scale diagram could show this clearly, but I suggest that the photographic evidence is sufficient to put the issue beyond dispute.

I will add one last comment: the Apollo 15 Mission Report states: "The crew also reported that the buckling seemed to be uniform around the skirt periphery and that the exit plane height above the surface was uniform." I would be interested to learn if anyone can find any relevant dialogue or comment in the ALSJ, or the Debriefing Report, or elsewhere. I can find no corroboration for that statement, and I must suggest that the photographic evidence suggests otherwise.

LM-12
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posted 01-04-2015 07:02 PM     Click Here to See the Profile for LM-12     Edit/Delete Message   Reply w/Quote
Impressive bit of research there.

One thing I did notice: the NASA document stated that the buckling was "not due to the nozzle making contact with the lunar surface". The Mission Report stated that the buckling was "not due entirely to contact of the nozzle skirt with the lunar surface". Bit of a difference there.

Found an even larger version of AS15-88-11882, if that helps.

LM-12
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posted 01-05-2015 05:41 AM     Click Here to See the Profile for LM-12     Edit/Delete Message   Reply w/Quote
Some good views of the Apollo 16 and Apollo 17 engine bell clearances can be seen in these high-res versions of photos AS16-113-18330 and AS17-147-22517.

nasamad
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posted 01-05-2015 11:34 AM     Click Here to See the Profile for nasamad   Click Here to Email nasamad     Edit/Delete Message   Reply w/Quote
Thanks Geoffrey (Blackarrow), you have summed up pretty much what I was trying to get across, but with better grammar and more research.

I think it's pretty obvious from the enhanced image that the buckling was caused by an impact rather than internal pressure. It looks like an upturned plastic cup that has been pressed down on. I'm sure either the 16 or 17 crew talked about splitting the bell if it got too much pressure in it, rather than buckling it.

Blackarrow
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posted 01-05-2015 05:52 PM     Click Here to See the Profile for Blackarrow     Edit/Delete Message   Reply w/Quote
Good points by LM-12, and the Apollo 16 image is much clearer than the one I used (and makes the point better).

LM-12
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posted 01-06-2015 06:42 AM     Click Here to See the Profile for LM-12     Edit/Delete Message   Reply w/Quote
A recently-read LM landing gear abstract mentions the engine skirt. It is in this list of landing performance requirements for the landing gear:
  • provide sufficient energy-absorption capability at touchdown
  • provide adequate toppling stability at touchdown
  • provide sufficient clearance on lunar surface to avoid impact of descent-stage structure, tanks, and plumbing (descent-engine skirt allowed to crush on surface contact)
  • maintain tilt angle within specified limits for ascent stage lift-off


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