Spacelog Apollo 8

People listening to the high bit rate down here say it's like sitting in your living room listening to good hi-fi.

Sounds like a good idea.

Apollo 8, Houston. Coming up on 2 minutes to LOS. We got a good reservice on the primary evaporator, and everything is still looking very good down here.

Okay. Thank you.

Apollo 8, Houston. One minute to LOS. Are you still reading us loud and clear?

Loud and clear. Loud and clear.

Okay, fine. We've been noticing a little bit of increase in our background noise as you approach backside.

Roger. We had to go off the high gain. That's why.

Roger.

Have a good backside; we'll see you next time around.

Apollo 8, this is Houston. Over.

Houston, Apollo 8. Go ahead.

Roger. Read you loud and clear. Welcome back.

Roger. Looks like the evaporator—looks like the evaporator is holding okay, or at least it is trying to. It dropped the temperature down to about 32, and now it's come back up again and stabilized at about 42 degrees.

Roger. Copy you, Bill.

Houston, Apollo 8.

Apollo 8, Houston.

Roger. Houston, this is Apollo 8. What we are doing on the control point tracking—I managed to look for a CP-1 at the same time we were trying to do a CP-2 on this rev. I picked up two marks which are just as small, but more easily recognizable, than the ones that were given to me. I know that I can repeat the process and pick the same small point on the next rev. Now I can try to look for the control points that are written down, but I think that I have better control over the ones that we have.

Roger, Jim. Understand. We'll check that for you.

Roger. One more point: the control point times which you have given me are a little bit off, and I can notice by comparing these maps that these maps are not too well aligned either.

Roger. These two small points that you can repeat your marks on: will you be able to identify those precisely on a map? Over.

That's affirmative; that is why I picked them. They are both—they're both very prominent features, and they are both very small craters about the same size as the ones we are looking for, but I can pinpoint them on a map.

Roger.

Houston, Apollo 8.

Apollo 8, Houston. Over.

Roger. One more comment: as it offered a lot of controversy at data priority meetings, it looks like 10 degrees pitch up is the best attitude to obtain the horizon so that you can follow the landmark down through the scanning telescope. If you pitch down any more, full up trunnion will not get the horizon, and the horizon is a great help in leading yourself into the control point.

Roger. Understand.

Apollo 8, Houston.

Go ahead.

Jim, we concur with your use of the two small craters which you can repeatedly mark on and find on the map; and also if you will give us your new latitudes and longitudes, we can compute for you a time of closest approach to those points with the spacecraft 10 degrees pitched-up. Over.

Roger, Houston. CP-1 latitude minus 606269, longitude over 2, minus 78954, altitude plus 00152; for CP-2 latitude minus 09638, longitude over 2, plus 81691, altitude minus 00007. I tried to get CP-3 at the same pass, but I let it go by to get set up for this first track at the landing site.

Roger, Houston. CP-1: would you say again the latitude, and on CP-2, say again the longitude CP-2, please?

Roger. CP-1 latitude minus 06269; that is the latitude; and for longitude over 2 for CP-2, plus 81691.

Okay. We copied them. Thank you.

And it appears that resolve medium is a very good combination to track.

Roger. I understand. Resolve medium.

And it appears so far, Houston, that no spacecraft pitch motion is required to get five marks on the target in plenty of time.

Apollo 8, Houston.

Go ahead.

Go ahead, Houston.

Roger. I am about 15 minutes early with the TEI fix update and the map update. I will have them here whenever it's convenient for you to copy.

Apollo 8, Houston.

Go ahead.

Roger. We would like to ask you to stop using AUTO OPTICS on the pseudo landing site. It's necessary that we send you up a P27 to update the RLS values stored in the computer. Over.

Roger. I found … I went to MANUAL OPTICS on B-1.

Okay, Bill. Before we read the big TEI update here, I'd like to give Jim briefly a procedure for P22. When he comes to NOUN 89, we request that he do a VERB 34 ENTER. Do not proceed, and by so doing then, he will not incorporate the lat and longitude from his mark, and he will not change the reference value of the landing site, and we will solve this AUTO OPTICS problem. Over.

Let me see if I have this correct, Mike. When flashing 0689 comes up with the latitude and longitude information, I will not proceed but will go to VERB 34 and terminate. Is that correct?

Yes, that is affirmative. Do a VERB 34 ENTER instead of a PROCEED. And that will -

Alright. Is this technique true -

Houston, is this technique true for both the node control point AUTO OPTICS on P25?

Stand by one, Jim.

And the LM …

That is affirmative, Apollo 8. That is always true.

Okay. Roger. True for the code AUTO OPTICS and no landmark. I'll proceed instead of going on—or I'll use 34 instead proceeding on 89.

Roger. Thank you, Jim, and I have the TEI 6 hour when you are ready—or TEI number 6.

Go ahead.

Ready to copy.

Roger. I'm glad you are ready to copy TEI number 6. I've got one last comment for Jim before you do so. The VERB 89—or correction—the NOUN 89 we are talking about is the one that he gets after marking. There are two NOUN 89's, one prior to marking and one after, and our procedure references NOUN 89 after marking. Over.

Roger. Understand.

Thank you, and, Bill, you still ready to copy?

Ready to copy, Mike.

TEI 6, SPS/G&N: 45701, minus 040, plus 157. Are you with me so far?

Roger.

081:21:24.43, plus 31776, minus 00823, minus 01365 180 016 001, not applicable, plus 00188. Are you still with me? Over.

That's Roger.

Good. 31816 302 31624 40 2699 396 033, down 054, left 21, plus 0810 control minus 16500 12968 36222 146:42:04; GDC align remains the same; Sirius and Rigel, roll 129, pitch 155, yaw 010, ullage four quads for 15 seconds; horizon on 6-degree line at TIG minus 3 minutes. Over.

Roger, Houston. TEI 6, SPS/G&N: 45701, minus 040, plus 157 018:21:24.43, plus 31776, minus 00823, minus 01365 180 016 001, NA, plus 00188 31816 302 31624 40 2699. Are you with me?

Yes, I'm with you, Bill.

396 033, down 054, left 21, plus 08 10 minus 16500 12968 36222 146:42:04; same GDC align; Sirius and Rigel, 129 155 010, four jet, 15 seconds, horizon 6 degrees, TIG minus 3. Over.

Roger, Bill. On your ignition time, GETI is 81 hours, 081. Over.

Roger. Got it, 081.

Thank you, sir.

Thank you, Michael. As a matter of interest, these side windows are so hazy that when the sun shines on them, they just about—they are real poor for any visual observation or photography—heads-up.

Roger. Understand.

Apollo 8, Houston. Over.

Go ahead, Houston.

Roger. The last state vector updates we sent you, Jim, was to the LM slots, and you will have to transfer that over to the CSM slots using VERB 47 ENTER. Over.

Roger. Will do.

Thank you.