- Ken Mattingly (CAPCOM)
-
Wilco, Apollo 8. First, if you can spare, we would like to have the high gain to complete the dump.
- Ken Mattingly (CAPCOM)
-
Apollo 8, while we are waiting for the high gain, I will continue the trajectory summary. We can still get back to the mid-Pacific line in 146 hours from the thirteenth REV, and you are on your way after 138 seconds of the burn. That's 138 seconds, gets you clear of the butterfly region. We recommend not trying preignitions or restarts after 20 seconds. If you go beyond 20 seconds, this may get the trajectory beyond the correction—RCS correction capability to a free return. The weather in recovery area is good. We have an AOS following TEI of 89 plus 28 plus 39 and an AOS without TEI of 89 plus 37 plus 24. During the burn, you may notice a slight change in chamber pressure and tank pressures due to the fuel exhaustion in the storage tank and going to the sump tank. This may occur somewhere around 2 to 5 seconds into the burn. It'll be a small change in pressures in both systems. Going down the systems, all systems are GO. In ECS, we want to stop water boiling after TEI for trajectory purposes. Your water dump situation looks good; you should be good to greater than 105 hours. We'll try to hold off the water dump until after MCC 5. In the EPS, we'd like to stir the cryos prior to TLI—correction TEI. The next purge on the fuel cells will occur at approximately 92 hours, and that will be both hydrogen and oxygen. Your battery status: battery A 34.9, battery B 39.1, and Charlie 38.5. We have the single tank cryo capability. SPS: looking at the performance on the previous burns, you can anticipate a normal burn taking approximately 3.7 seconds in excess of the computed values. Engine performance looks nominal, and all parameters have been steady. RCS looks good; all four quads according to the computer programs have approximately the same capacity. You have a good REFSMMAT to take you through TEI. We'll have a post TEI PTC attitude for you in a few minutes. and that just about wraps up what we have on systems. Over.
- Frank Borman (CDR)
-
Roger. Thank you, Houston. We appreciate the summary. We're trying to get high gain.
- Frank Borman (CDR)
-
You do have the high gain. Now, Ken, as I understand it, if it shuts down after 20 seconds of burn, you don't want us to try to re-light it. Is that what you said?
- Frank Borman (CDR)
-
Okay. You want me to start it on tank A and then switch to B again like we did on our LOI, right?
- Ken Mattingly (CAPCOM)
-
Apollo 8, that's negative. We had not uplinked this PAD. We'll put this one in on the next pass.
- Ken Mattingly (CAPCOM)
-
Apollo 8, Houston. We have completed the tape dump, and the recorder is yours.
- Ken Mattingly (CAPCOM)
-
Apollo 8, Houston. We're 5 minutes to LOS; we'll have AOS Honeysuckle at 87:38:42.
- Frank Borman (CDR)
-
Roger, Ken. Thanks a lot. We'll see you around the next pass. Just have our TEI update for us when you're ready. Okay?
- Ken Mattingly (CAPCOM)
-
Apollo 8, we would like to have the high gain, and when we get that, well, we will start a dump, and we will start your updates.
- Ken Mattingly (CAPCOM)
-
Alright. TEI 10, SPS/G&N: 45597, minus 040, plus 157 089:19:15.67, plus 35186, minus 01512, minus 00520 180 007 000, November Alfa, plus 00186 35223 318 35018 42 0924 253; Scorpii Delta, down 069, left 45, plus 0748, minus 16500 12994 36300 146:50:05; primary star Sirius, secondary Rigel, 129 155 010; four quads, 15 seconds, ullage; horizon on 3.2-degree window line at T minus 3; use high-speed procedure with minus Mike Alfa. Over.
- Ken Mattingly (CAPCOM)
-
Apollo 8, we would like to have you go to P00 and ACCEPT and we would like to take the recorder at this time; then I will copy your PAD.
- Jim Lovell (CMP)
-
TEI 10, SPS/G&N: 45597, minus 040, plus 157 089:19:15.67, plus 35186, minus 01512, minus 00520 180 007 000, not applicable, plus 00186 35223 318 35018 42 0924 253; Scorpii Delta, down 069, left 45, plus 0748, minus 16500 12994 36300 146:50:05; Sirius, Rigel, 129 155 010; four-quad, ullage, 15 seconds; horizon on the 3.2-degree mark is T minus 3; high-speed procedure minus MA.
- Ken Mattingly (CAPCOM)
-
Roger. TEI 11, SPS/G&N: 45597, 0—correction—that's minus 040, plus 157 091:18:12.24, plus 36325, minus 01727, plus 01428 180 003 000, November Alfa, plus 00186 36394 323 36186 42 0995 254; Scorpii Delta, down 103, left 48, plus 0742, minus 16500 13005 36327 146:51:44; Sirius and Rigel, 129 155 010, four quads, 15 seconds; horizon on 2.9-degree line at T minus 2; high-speed procedure with minus Mike Alfa. Over.
- Jim Lovell (CMP)
-
Roger, Houston. TEI minus 11, SPS/G&N: 45597, minus 040, plus 157 091:18:12.24, plus 36325, minus 01727, plus 01428 180 003 000, not applicable, plus 00186 36394 323 36186 42 0995 254; Scorpii Delta, down 103, left 48, plus 0742, minus 16500 13005 36327 146:51:44; Sirius, Rigel, 129 155 010; four quads, 15 seconds, 2.9-degree window mark at T minus 2; high-speed procedure minus MA.
- Bill Anders (LMP)
-
Houston, could you give me the SPS helium tank temperature at about 87:20, please?
- Ken Mattingly (CAPCOM)
-
Apollo 8, Houston. At 87:48, we're reading 84 degrees, and at LOS we had 80. We'll take a look at the tape and see if we can find out what we had on the backside.
- Ken Mattingly (CAPCOM)
-
Okay, Apollo 8. We've reviewed all your systems. You have a GO for TEI. One of the things we would like to do as soon as you come out on the other side is a P23. We are checking into your helium pressures now. We're going to correlate not only the last REV but the previous REV for the same location, and we will have that number for you in a little bit.
- Ken Mattingly (CAPCOM)
-
Affirmative. And looks like that will go with the entry REFSMMAT; begins at 92 hours.
- Ken Mattingly (CAPCOM)
-
Okay. On the helium tank TEMP's: that's not recorded on low bit rate, and looking over our tape dumps, most of this stuff we have on the backside there is low bit rate. So we won't be able to give you an exact number, but looking at what we have every time we go out of sight and come back over the hill, it looks like you can expect about 82 to 84 degrees as a nominal temperature.
- Ken Mattingly (CAPCOM)
-
Apollo 8, Houston. We'd like to have the tape recorder for about 5 minutes for one last look.
- Ken Mattingly (CAPCOM)
-
Thank you. And I guess we still have a cryo stir ahead of us, and we've checked your triple bias, and there's no change.
- Frank Borman (CDR)
-
We're on a maneuver to burn attitude, and it's going to make us lose the high gain.
- Ken Mattingly (CAPCOM)
-
Apollo 8, the tape recorder is yours. We have your double umbra update, 89:07:15.87.
- Ken Mattingly (CAPCOM)
-
Apollo 8, Apollo 8, this is Houston. Three minutes LOS; all systems are GO. Over.
- Jim Lovell (CMP)
-
That burn status report: it burned on time; burn time 2 minutes 23 seconds, seven-tenths VGX. Attitude nominal, residuals minus five-tenths VGX plus four-tenths VGX—of minus O VGZ. DELTA-VC minus 26.4.
- Jim Lovell (CMP)
-
Roger. We had 2 minutes 23 seconds. Our—wait one. Change that to read 3 minutes 23 seconds.
- Ken Mattingly (CAPCOM)
-
Apollo 8, at the first convenient moment, we'd like to have the high-gain antenna.
- Ken Mattingly (CAPCOM)
-
Apollo 8, Houston. We do not have any data on the ground yet; the voice is very good.
- Ken Mattingly (CAPCOM)
-
Apollo 8, Houston. We'd like to try to have you manually acquire on the high gain.
- Ken Mattingly (CAPCOM)
-
Roger. Reading you loud and clear. Initial tracking indicates a 4 foot per second at 8 hours will put you on target.
- Ken Mattingly (CAPCOM)
-
Go ahead, Apollo 8.
Expand selection down Contract selection up
Spoken on Dec. 25, 1968, 3:18 a.m. UTC (55 years, 10 months ago). Link to this transcript range is: Tweet