Otrobonita/noicy-space-talks huggingface dataset:
CC: - - GET of 75 plus 33. RCS total, 83 percent; quads, in order, 83, 83, 82, 84 percent; hydrogen, 72.4, 72.8; oxygen, 89, 87, and 38.
LMP: Houston, 14. Do you read me?
CC: Roger, 14. Reading you loud and clear now. We had another antenna switch. Over.
LMP: Roger. I lost you after the first hydrogen tank.
CC: Okay. Hydrogen tank l, 72.4, 72.8; oxygen, 89, 87, 38. Over.
LMP: Roger. I got your ...
CC: Say again your last, Ed.
LMP: Roger. I only got the first oxygen tank. Try me again on 2 and 3.
CC: Okay. Tank 2, 87 percent; tank 3, 38 percent. Over.
LMP: Roger. I got 75:33; RCS total, 83; quads are 83, 83, 82, 84; hydrogen, 72.4 and 72.8; oxygen, 89, 87, 38.
CC: Roger. Are you all eating breakfast up there now?
LMP: Our - We're starting. The cooks are in the kitchen at the moment. Our radiation readings for last night - or rather for this morning are 16045 for Al, 1042 - 01042 for Stu, and 05038 for Ed.
CC: Roger. 16045 for Al, 01042 for Stu, 05038 for Ed, and how about quantity of sleep? Do you have any comments on that? Over.
LMP: Roger. For Al, 6 hours; Stu, 6-1/2; and for Ed, 6-1/2.
CC: Roger, Ed. And Ed, when you - when you all feel prepared, we've got quite an extensive batch of paperwork to pass up to you here.
LMP: Okay, Bruce. Stand by 1.
LMP: Is it all going to be associated with the flight plan?
CC: Well, let's see. We got - we got a comment on the Tephe m. We've got a flight-plan update. We've got a docking probe status report. We've got a pericynthion plus 2 abort pad. We will have an L0I abort chart in numbers - criterion update. We'11 have some questions for you on the cosmic ray flashes. And when it comes in, we'11 have a procedure for you for checking out the ascent stage battery number 5 in the _. Over.
CC: Also the sports news and commentary on midcourse 4.
LMP: Okay. Why don't we get the flight plan first, so that we cmn kind of see where we're going. And then we'11 string the others out throughout and after breakfast.
CC: Okay. Actually, I think you were looking over my shoulder, because the flight-plan update is about the simplest of the whole bunch. What we're aiming towards here - -
LMP: We are looking over your shoulder.
CC: (Laughter) What we're aiming towards here is get- ting you into the LM shortly after midcourse cor- rection 4 - to do a little more systems detective work on ascent battery 5. Make everybody feel a little warmer down here. And, of course, the rest of the LM is still in 4 0 shape. At 76 hours in the flight plan, we'd like you to pressurize the LM as required. Over.
LMP: Okay. 76 hours, pressurize the LM as required.
CC: Roger. At 77 hours, plus 45 minutes, which is right after midcourse 4, mRneuver to Moon-view attitude. And that attitude is presently contained in the flight plan at 78 plus 55 and is roll 352, 110, 311. 0ver.
LMP: Roger. Maneuver to Moon-view attitude, and say again the angles. I understand that's at 77:45, right after midcourse 4.
CC: Roger. Angles are 352, 110, 311, and they're currently in the flight plan at 78 plus 55.
CC: You still there, Ed?
LMP: That's affirmative. Okay, I have moved it from 78:55 to 77:45.
CC: Roger. And this is a good attitude for LM com- munication on AFT OMNI. And the procedure that we'11 have for you later on will have the S-hand up for telemetry but not for voice, so you want to use AFT OMNI? At 78 hours, or from 78 hours to 80 hours even, we have blocked out for LM check- out of the ascent batteries so you can plan on IVT to the LM at about 78 hours and be back out by 80. Over.
LMP: Okay. Understand that the attitude we're going to is good for the LM AFT OMNI, and we will IVT to the LM at 78 hours for a battery-5 checkout and be back - plan to be hack by 80 hours.
CC: Roger. And meanwhile, back in the command module, Stu can press on with the rest of the normal com- mand module activities, such as the P52 and all that.
LMP: Okay. You're going to have some good words on the ascent battery 5 for me, you say, in a little while.
CC: Yes, indeed. Joe Engle was Just over in the LMS here in Houston running through the thing, and it's a fairly - fairly long procedure as far as hand- writing goes, but relatively straightforward, and we'11 cover it for you in detail.
CC: Would you like a general breakdown on what we plan to do?
LMP: I'11 stand by until you're ready to read it out, but maybe you can give me a s_mmary before.
LMP: Okay. Ready for the next item.
CC: Okay. This is the docking probe status summary. The conclusion down here is that, on your final successful attempt, the probe's spring started to compress slightly, followed by capture latch en- gagement. And the dock latch went barber pole, and then the bottle fired and retraction was nor- mal, although the time was somewhat shorter due to the continued firing of the service module RCS. The talkback operation during initial extension and final docking plus the accelerometer data, the capture latch release mode occurrence during the extensions, all indicated normal extension, capture, and retract sequence. Some consideration was given to the possibility that the RCS thrusting compressed the probe until the docking latches engaged, but this would have required more force than the RCS provides. As we mentioned yesterday, we are still GO for the mission. Over.
LMP: Okay. And I think I'd like to have you repeat that after A1 and Stu get on the headsets so that I won't have tow rite the whole thing down. I think they'd like to hear it.
CC: Okay. How about a pericynthion - -
CC: Okay, Ed. We're getting a lot of noise on the downlink right now. Let's stand by until after we shift antennas again.
CC: Okay, 14. How do you read now?
LMP: Loud and clear, now, Bruce. Okay, our status at the moment - we're going to hold the probe report until A1 and Stu get on the headsets. Let's press on. What's the next thing you have?
CC: Okay. Pericynthion plus 2 abort pad, standing by; P30.
CC: Are you ready for the P30 pericynthion plus 2, Ed?
LMP: Okay. LOI plus 2.
CC: Roger. Pericynthion plus 2 abort pad. SPS/G&N, 63, 300, plus 0.90, minus 0.33; Tig, 084:35:20 - -
LMP: Bruce, hold it a minute.
LMP: Okay. Would you start over again now for me, please?
CC: Wilco, Ed. This is a pericynthion plus 2 abort pad. SPS/G&N, 63, 300, plus 0.90, minus 0.33, Tig, 084:35:20.03, minus 0711.5, minus 0053.1, minus 1276.8, roll N/A, 084 pitch, yaw N/A. The rest of the pad is N/A. This is an SPS docked burn and the attitudes are based on the landing REFSMMAT. site Read back. Over.
LMP: Okay. It's pericynthion plus 2. SPS/G&N, 63, 300, plus 0.90, minus 0.33, 84:35:20.03, minus 0711.5, minus 0053.1, minus 1276.8, roll N/A, pitch 084, yaw N/A, or is that 000. The rest of the pad is N/A. SPS docked, landing site REFSMMAT. Over.
CC: Roger. I now have your midcourse-4 pad. I - I think you're losing ground on me down here. They seem to be piling up faster than we can get them read up.
LMP: Okay. Bruce, on the angles on that one. The roll N/A, was pitch was 84, and yaw was zero. Is that correct?
CC: Yaw was N/A. Actually, if you want the numbers, roll would be 356 and yaw would be 009. We under- stood there was a previous agreement that you were Just going to use pitch for checking, and you would take the roll and yaw as computed by P40. Over.
LMP: Okay. Ail right, press on.
CC: Okay. Let me hold off on this midcourse-4 pad a minute. I can give you just a second's worth of discussion on the thing. It's coming out to 3.8 feet per second, and this is very close to your SPS minimum impulse. It'11 be 0.69 seconds of burn time compared to your guaranteed 0.50 rain impulse, and when you get down to DELTA-V the c 2/10ths value of is what they want set in the counter. Over.
LMP: Okay. Understand that. SPS/G&N,
CC: Okay. Midcourse correction number 4. 63, 375, plus 0.90, minus 0.33, Tig, 077:38:13.98, minus 0001.6, minus 0002.8, plus 0002.1, roll 0il, 249, 325, NOUN 44 N/A, DELTA-V T 0003.8, 0:01, 0000.2, sextant star 01, 173.2, 33.5, GDC align Sirius and Rigel; 230, 170, 002, no ullage; HIGH-GAIN ANTENNA angles, PITCH plus 32, YAW 290, NARROW BEAM, AUTO- MATIC mode. Read back. Over. SPS/G&N,
LMP: MCC-4, 63, 375, plus 0.90, minus 0.33, and 077:38:13.98, minus 0001.6, minus 0002.8, plus 0002.1, plus - or rather 011, 249, 325, N/A, NOUN 44 0003.8, 0:01, 0000.2, 01, 173.2, 33.5, Sirius, Rigel at 230, 170, 002, no ullage, HIGH- GAIN ANTENNA angles, PITCH plus 32, YAW 290; you want it on NARROW and AUTO.
CC: 14, Houston. Readback correct.
LMP: Houston, 14. How do you read now?
CC: Okay. When you have a chance we'd like POO and ACCEPT Ed. And we'11 uplink you the midcourse-4 target load and a new state vector. Over.
LMP: Okay, Bruce. You have POO and ACCEPT.
CC: Okay, Ed. You may recall our discussion on T ephem last evening, with regard to the sign of the quan- tity in R 3. We've had a request down here that you, and on the CMC LGC, load in the T from the pad ephem that we passed you. That is the - the quantity using all positive signs. Do you still have that handy?
LMP: Let me doublecheck.
LMP: Roger. Those are the numbers 00006, 39223, and 16020. Is that affirmative?
CC: Roger, that's the one.
LMP: Okay, we'11 load these in after while.
CC: Let us finish with the uplink first.
CC: Okay, Ed. We have a - a rather detailed change to the LOI Mode I DPS abort chart and numerical data. This is found in the flight plan in the Contingency Checklist, and the numerical stuff is on one of your cue cards. It'd probably be easiest if you broke out the flight plan, say, and went through it with me.
LMP: Okay. Did you get my readback on the midcourse-4 pad?
CC: Uh - -
LMP: It sounded to me like you dropped out before I finished reading it hack.
CC: Yes. As far as - as far as I can tell, I got all of it. I recall definitely down through Sirius and Rigel, and I believe I recall your reading the HIGH-GAIN ANTENNA angles back, and I got - so I'11 Roger for that.
LMP: Okay, Bruce. Give me a few words on the DPS abort changes before we start giving the actual numbers.
CC: Okay, you have a change in the DPS DELTA-V avail- able line due to a different engine model, change in the spacecraft weight, and a change in the usable propellant from the time that this curve was calculated. You have a change in the two other lines, which are the LOI plus 2-hour and LOI plus 30-minute abort DELTA-V based on the change in your obit from the nominal plan. This all backs up to the 40-minute-late lift-off. And the numer- ical changes are a consequence of that, also. Over.
LMP: Okay. Let's start through them slowly then and see if we can correct them.
CC: Over here in the DPS DELTA-V available line, the left-hand intercept is at abort DELTA-V of 1966 feet per second at L0I DELTA-V of zero. The right-hand intercept on the vertical dashed line comes at an abort DELTA-V of 2130 and the L0I DELTA-V of 725. Then connect the two intercepts together with a straight line. Over.
LMP: Okay. Stand by. The first one is 1966. Let's just take them one at a time, and I'11 plot them.
LMP: And you say the - the right-hand intercept is 21 what ?
CC: Is 2130, 2130, and it falls on that vertical dashed line at 725. It separates Mode I from Mode II.
CC: Okay, connect them up.
CC: 14, Houston. The computer's yours.
LMP: Okay, I'm in BLOCK. Give me the next llne now.
CC: Roger. In the LOI plus 2-hour abort DELTA-V re- gion, the left-hand intercept is at 1477 feet per second. Over.
LMP: Copy, 1477.
CC: Roger. And the right-hand end point is at 2026 abort DELTA-V, and LOI DELTA-V of 238. It should intercept your DPS DELTA-V available line where it crosses the boundary between the Mode I 2 hour and the Mode I 30 minutes. Over.
LMP: Roger. Took care of that, and let me draw that one.
CC: Okay. You ready for the next one?
LMP: Okay. Ready for the next one.
CC: Okay. Over in the LOI plus 30-minute abort region, the left-hand intercept, with the boundary between Mode I 2 hour and Mode I 30 minutes, occurs at abort DELTA-V of 1517 and L0I DELTA-V of 238. Over.
CC: And we're going down in the mud again, Ed. I'm going to wait for the antenna changeover before we continue with that one.
LMP: Okay. I've got you at 1517 for the first one.
CC: Okay, 14, Houston. We're coming back in now. I confirm 1517 for the left-hand edge, and the right- hand intercept is at abort DELTA-V of 2395 on the 725 DELTA-V magnitude dashed line. Over.
LMP: 2375. Is that correct?
CC: Negative. 2395. Over.
LMP: Okay. 2395.
LMP: Okay, Bruce. Have that line plotted.
CC: Okay. And all three of those lines ought to be pretty close to parallel to the existing lines; you concur?
LMP: Yes, they sure are.
CC: Okay. Over to the numerical data. Come on over to the - the little block there and, on the second line down under burn time starting out with 0 plus 33, Mode I, loose, it should be zero plus 33 through 1 plus 19, and DELTA-V M is 238 through 570. Over.
LMP: Okay. The burn - the burn - burn time from 033 to 115 should be 033 to 119, and the corresponding DELTA-V M is 238 to 570.
CC: Roger. Next line down. The burn time is 1 plus 19 through 1 plus 40, and the burn time is - or the DELTA-V M is 570 through 725. Over.
LMP: Okay. We change from ll9 to 140 and DELTA-V M is 570 to 725.
CC: Roger. On the next line down, you change i plus 39 to i plus 40, so it reads i plus 40 through 2 plus 41. Over.
LMP: Okay. One - The next line is 140 to 241.
CC: Okay, now down below it, you've got a colt,mn for updated times. And I'11 read you the updated times.
CC: Okay. GET of LOI ignition: 82 plus 36 plus 47, 83 plus 06 plus 47; roll: 127, 264, 348; CSM IMU angles GET abort ignition, 84 plus 36 plus 47. The next block down under LM FDAI angles, the T. : 84 plus 36 plus 47; 170, 261, 000. zg
LMP: Okay. And Bruce, the only time I think I've missed is the CSM IMU angles at LOI plus 30.
CC: Okay. 83 plus 06 plus 47. Over.
LMP: Okay. I read back GET and LOI ignition update is 82:37:47; the LOI plus 30 is 83:06:47; CSM IMU angle for LOI plus 2 is for a time of 84:36:47; and the LM angles for that time are - the LM FDAI angles for that time are 80 - 84:36:47; and they're 170, 261, 000.
CC: Okay, Ed. The readback is correct except that you under omitted the roll, pitch, and yaw angles CSM IMU angles for LOI plus 30.
LMP: Roger. I didn't hear them. Are they - they the same?
CC: Okay. Roll and yaw are the same. Pitch has changed from 263 to 264. Over.
LMP: Oh, those. Okay, I thought I read them to you, Bruce. I have them: 127, 264, and 348.
CC: Roger. Readback is correct, and we've got some news whenever you're ready.
LMP: Okay. Let's hold off and let the other guys get on the headsets and have some news, while I get some breakfast.
CC: Okay, and those changes need to be made in the Contingency Checklist, the flight plan, and on your cue card.
LMP: Roger. We'11 do it.
CC: Apollo 14, this is Houston. We would like you to reload Tephe m prior to midcourse 4; over.
CMP: Okay, Bruce; we'11 reload Tephe m. I'11 do that right now. And the DELTA-V test went real well, and the null bias check with a minus 100 at the :_tart, and went to a minus 98.4.
CC: Did you say 98.4, Stu?
CMP: That's affirmative; 98.4.
CMP: Okay, Bruce, I reloaded. And there it is if you'd like to check it and make sure we're all squared away.
CC: Okay, stand by. Roger, we concur, Stu; it looks good.
CC: Apollo 14, Ed. This is Houston. Do you have a copy of the LM Activation Checklist in the command module at this time, or did you leave both of them in the LM? Over.
LMP: Yes, I've got them - -
CDR: We have them here in the command module.
CMP: Okay, Bruce. The torquing angles are on the DSKY, and I'11 be torquing at 76:51:30.
CC: Okay. It looks good from down here, Stu.
CMP: Okay, Bruce. Looking over the flight plan, we moved up that maneuver to the Moon-view attitude, and I'm going to go the way I did back here right after midcourse 4 instead of where it shows over at 78:50 if you all agree.
CMP: Okay. The pad value for DELTA-V is 0.2, and c you all gave us that before we ran our null bias check. Is that - is that still a good value?
CC: Yes, that's still a good number, Stu.
CC: Okay. We'd like to get the high gain, whenever you can crank it up.
LMP: Houston, 14 on the high gain. How do you read?
CC: Okay. Your high gain is oscillating a bit there. Want you to try another acquisition there, Ed?
LMP: Roger, Fred. We've tried it twice, and it's still doing it. I'11 give it one more go.
LMP: Houston, 14. That seems to be the best we could do. It's still oscillating. Got another sug- gestion?
LMP: 14, Houston.
CC: Okay, Ed. Suggestion is to take the SERVO ELECTRONICS switch, panel 2; go to SECONDARY; and then try REACQ.
LMP: Okay, Houston. I think we've finally got it up on the fourth attempt.
CDR: Okay, Houston. We got about 40 seconds to burn. We're ready to go on time.
CDR: Okay, we had a good burn.
CDR: Okay, Houston. 14 with a burn report.
CDR: DELTA-V minus 2.6; and the fuel and oxidizer, C' no appreciable change.
CC: Okay DELTA-Vc, minus 2.6; and the fuel/OX, no change.
CC: We would like AUTO on the HIGH GAIN now, Ed. And just one other question. Did you mean you tried four times on the SECONDARY SERVO ELEC- TRONICS to get locked up?
LMP: Yes, it was about that, Fred. It could be that I wasn't giving it enough delay time before I tried something else when it was in the NARROW position. But I thought I was, and I don't know what I did differently on the last attempt that did work than the previous attempts which didn't work.
LMP: Roger. I went from WIDE to MEDIUM to NARROW.
CC: Okay. LM/command
CDR: Houston, 14. The module DELTA-P is zero. We're starting to remove the tunnel hard- ware.
CC: And are both A1 and Ed on the headsets now?
CC: Okay. Looking at - -
LMP: Yes, we're all on, Fredo.
CC: Okay. Looking at the procedure here for the business in the LM, looks like the better way to handle it, rather than have you write it all down, is for me to just give it to you on a step-by-step basis after you're in the LM and set up and ready to go. And I'11 just have somebody, Joe here, checking me off as we do it.
CDR: Okay. We'11 let you know when we're in there, and we'11 keep command module comm in there.
LMP: Just a quick comment in passing. The Moon is out my rendezvous window right now, and it seems to be growing noticeably in size. We've reached that point where the - we're running downhill very rapidly toward it.
CC: Roger, Ed. Showing you about - oh, it looks like about 205,000 out, now.
CMP: Hey, Fred, old boy, this Moon-view attitude is just what it says. It's got her framed right in the hatch window.
CC: Incredible.
CMP: Yes, that's just like everything else. You all do good work.
LMP: Okay, Fredo. I'm through the tunnel and ingres- sing the LM at this point. What's about the first thing you want me to head for?
CC: Okay, I'11 let Joe talk to you here and kind of give you a few words on the big picture. And then we'11 start in.
MCC: Okay, Ed. What this is going to amount to is an abbreviated - a very abbreviated powerup, and we will transfer to LM power; so, Stu, you can stand by, and we'11 get our own times on that. Now, Ed, if we have a comm problem any time during this - and we are out of configura- tion - just get the activation checklist and go to page 1-17 and complete the deactivation from that point on.
MCC: And, Ed, if you're ready to go now, we'11 start through here.
LMP: Okay, Joe. How about giving me a quick overall picture of the problem as you saw it from the ground. I didn't see much of anything here that was indicative of a problem.
MCC: Okay. Just a second here.
CC: Okay, Ed. I wanted to get the values correct 3/lOths here. TM picked up about of a voltage - of a volt iow on battery 5, which gave some concern, and, primarily, we Just want to verify that perhaps we're not - we don't have a gage that's giving us that much of a difference, rather than the battery itself.
LMP: 3/10tbs of a volt?
CC: Yes. That's affirmative. That's open-circuit voltage, Ed.
LMP: As I recall, we read - Roger. As I recall, we read them off a half a volt different, 36 and a half to 37. Is that right?
CC: Roger, Ed. That was half a volt onboard, and the telemetry showed the 3/10ths down here.
CC: Okay. And essentially, Ed, what we're going to do is put the - put both batteries on an open bus to read out both bus and battery volt- ages. And, if we're not satisfied with the readings at that point, we'11 go ahead and load up the LMP bus and - put a load on it rather - and then check the battery performance both by itself and sharing a load on the LMP bus.
LMP: Okay. I understand what you're going to do.
CC: Okay. Let's press on, and I'11 read the items off in checklist fashion. And I'11 read one or two items at a time, Ed, depending on if they're in the same proximity, and wait for your verification.
CC: Okay. Up front, let's turn the FLOODLIGHTS to ALL.
LMP: FLOODLIGHTS are at ALI..
CC: Okay. Window shades, down.
LMP: That's in work.
LMP: Okay. Window shades are down.
CC: Okay. And back on ECS panel now. The DESCENT WATER and DESCENT OXYGEN, both OPEN.
LMP: WATER and 02 are OPEN.
CC: CABIN REPRESS to AUTO.
LMP: CABIN REPRESS going to AUTO.
CC: And on panel 16, CABIN REPRESS circuit breaker, closed.
LMP: REPRESS breaker, closed.
CC: Okay. And, Kitty Hawk, we're ready to transfer to LM power now, and if you'11 give us the mark, we'11 get the time.
CMP: Okay, Joe, on my mark; 3, 2, 1
LMP: I have power.
CC: Okay, Ed. We've got it. And now on panel 11 and 16. The TRANSLUNAR BUS TIE breakers, both closed.
LMP: TRANSLUNAR BUS TIES are closed.
CC: Okay. On panel 11, SIGNAL CONDITIONER 1, closed.
LMP: CONDITIONER l's closed.
CC: Over on the other side on 16, SIGNAL CONDI- TIONER 2, closed.
CC: Okay. Under EPS, the DISPLAYS and the DESCENT ECA control, both closed.
LMP: Okay. EPS DISPLAYS and DECA - DESCENT ECA control, closed.
CC: Okay. Now verify the DESCENT BATTERIES, all four talkbacks are on LOW and the DESCENT BATTERY talkback is gray.
LMP: That's verified. That's verified. S-BAND,
CC: Okay. On panel 16, under COMM, PRIMARY both breakers, closed, and the PMP, closed.
LMP: Okay. COMM, PRIMARY S-BAND power amp TRANS- MITTER/RECEIVER and PMP, closed.
CC: Okay. And while we're doing this, you can keep your eye on that bus voltage - whether or not we need to go to high taps.
CC: Okay. Still on 16, the PCM/TE breaker, closed. PCM/TE,
LMP: closed.
CC: Okay. And on 16, ASCENT ECA and ASCENT ECA CONTROL, both closed.
LMP: Okay, ASCENT ECA, CONTROL, closed.
CC: Okay, Ed. Now, on your audio panel on the LMP side, S-BAND T/R to T/R.
LMP: S-BAND T/R, T/R.
CC: And under COMM, under the S-BAND, PM, PRIME, PRIME, OFF, PCM.
LMP: Okay, PM, PRIME, PRIME, OFF, PCM.
CC: Okay. And then OFF/RESET on your RANGE.
LMP: ... Okay. OFF/RESET, then 27 volts. Let's switch to high taps.
LMP: Okay, I'm on high taps.
CC: Okay. Very good. Now on your TELEMETRY, Ed, we'11 want OFF and HI.
LMP: And OFF and HI. You have it.
CC: Okeydoke. Now, on the S-BAND ANTENNAS, you might take a quick check and see which is your best OMNI there.
LMP: Well, since we don't have those meters powered up, I don't have anything to tell by.
CC: Okay. We've got data now, Ed. Thank you.
LMP: Okay. I'm on AFT.
CC: Okay, now stand by l; we'11 see if we're ready to press on here.
CC: Okay, Ed. We're ready to press on, and, for your information on telemetry here, we're still showing that ASCENT about 3/10ths of a volt low, ascent 5. Okay, Ed. We're ready to pick up now on panel 11. EPS CROSS TIE BALANCE LOADS, open.
LMP: Okay. EPS CROSS TIE BALANCE LOADS, panel 11.
LMP: Is open. That makes them both open, now.
CC: Okay. Now we're going to turn off BATTERIES 3 and OFF/ 4, so BATTERY 3 and 4 HI VOLTAGE to RESET. And you may get a dc feeder-fault light here. OFF/RESET.
LMP: BAT 3 and 4, you want the I have bos - both B__LANCE LOADS and BUS - CROSS TIE BUS, open. In other words, you want to dump the COMMANDER's BUS. Is that correct?
LMP: Okay. Here they go. And I have a feeder fault.
CC: Okay. You do have a feeder fault?
LMP: I have a feeder-fault light.
CC: Yes, that's what I mean. Okay. Very good. Now on panel 11, Ed, they want to open all the circuit breakers on panel 11, except SIGNAL CON- DITIONER l, the DC BUS VOLT, and both BAT FEED TIE breakers.
CC: Okay. I want them all open except SIGNAL CONDITIONER l, the DC BUS VOLT. Is that affirm?
LMP: Okay. It's open. We never got it closed. I'm closing it now.
LMP: Okay, Joe, I'm - Say again the ones you want closed.
CC: Okay, Ed. We have four that we want closed. They are the SIGNAL CONDITIONER - SIGNAL CONDI- TIONER l, BAT BUS VOLTS, and both BAT FEED TIE breakers.
LMP: Say, you're breaking up. Give me the last three again. I have the SIGNAL CONDITIONER, but I still don't get the last three.
CC: Okay. The DC BUS VOLTS and both BAT FEED TIE breakers.
CC: Okay. Both BAT FEED TIES, DC BUS VOLTS, and the SIGNAL CONDITIONER. I'm now pulling the RENDEZVOUS RADAR HEATER, the STANDBY breaker, ANNUNCIATING/ the LANDING RADAR HEATER breaker, DOCKING/COMPONENT lighting breaker, _ STANDBY, DESCENT ECA, TRANSLUNAR BUS TIE. I now have four bus - four circuit breakers closed, the remainder open.
CC: Okay. And you have the IMU STANDBY breaker open. Is that affirm?
CC: Okay, Ed. Our next step now. We'd like to bring BATTERY 5 BACK UP, ON.
LMP: Okay, BATTERY 5 BACK UP COMMANDER FEED is ON. !
CC: Okay, very good. And onboard there, if you'd compare both your battery and bus voltages and give us a readout, please.
LMP: Okay, BATTERY 5 is reading about 35.8, and the COMMANDER's BUS is reading 35.8.
CC: Okay, Ed. BAT 5 BACK UP, OFF.
LMP: BAT 5 BACKUP, OFF.
CC: Okay, Ed. BATTERY 6 NORMAL, ON.
LMP: BATTERY 6 NORMAL is ON.
CC: Very good, now give us battery and bus voltages, please.
LMP: Okay, I read 36 on the bus, 36 on the battery.
CC: Okay, Ed. Now, BATTERY 5 BACKUP to ON, and when you do it, see if BATTERY 6 pulls any of BAT- TERY 5 load.
LMP: Okay, stand by.
LMP: BATTERY 6 BACK UP, ON now. And, looks like the volt on - the voltage on 6 rose Just a little bit, and I see no change in current. It appears that it's sharing the load; they're both at 36 plus.
CC: Okay. Now let me verify, Ed. You do have BAT- TERY 5 on BACK UP and BATTERY 6 on NORMAL.
CC: Okay. Stand by 1 now, and let us look at the stuff here.
LMP: With your concurrence, I was looking at 6 when I brought 5 BACK UP, ON. Let me shift it - my POWER/TEMP TEMP MONITOR - MONITOR - and watch 5 and cycle them, if that's okay.
CC: Okay, Ed. First could you verify ASCENT ECA CONTROL breaker is closed, please.
CC: Okay. And the ASCENT ECA breaker, also.
CC: Okay. We'd like ASCENT ECA closed on 16, Ed.
CC: Okay, Ed. Now we'11 take - we'd like you to take BATTERY 6 to OFF momentarily and then back to NORMAL power, and you can watch BATTERY 5 voltage there on your monitor.
LMP: Okay, BATTERY 6 coming OFF.
LMP: Now when I cycle BATTERY 6, the BATTERY 5 voltage comes up when BATTERY 6 is brought on the line. It drops down when BATTERY 6 is off the line. However, by watching 6, I do not see any current drain.
CC: Yes, we concur. We're seeing the same thing here, Ed. And stand by just a moment in this configuration now.
CC: Okay, Ed, next function. Let's take BATTERY 5 BACK UP - correction - BATTERY 6 NORMAL FEED, OFF.
LMP: BATTERY 6 NORMAL is OFF.
CC: And BATTERY 5 BACK UP, OFF.
LMP: BATTERY 5 BACK UP, OFF.
CC: Okay, Ed. We can turn BATTERY 3 HI VOLT and BATTERY 4 HI VOLT back ON now?
LMP: Okay, BATTERY 3 HI VOLT is ON. BATTERY 4 RI VOLT is ON.
CC: Okay, Ed - -
LMP: ... 5 VOLTS.
CC: Okay, very good. Okay, Ed. If you have your activation - Do you have your activation check- list there with you?
CC: Okay, go ahead and configure panel 11 now as per page 1-3, and I'11 have four changes when you - when you get the breakers configured there.
LMP: Okay. Configuring panel 11 as per 1-3.
CC: Okay, Ed. And give me a call when you get panel 11 configured there.
LMP: Okay, Joe. It's complete.
CC: Okay, very good. Now I've got four breakers I'd like for you to change on 11. The CROSS TIE BALANCE LOAD breaker, open.
LMP: Okay. CROSS TIE BALANCE LOADS is open.
CC: TRANSLUNAR BUS TIE, closed.
LMP: TRANSLUNAR BUS TIE, closed.
CC: SIGNAL CONDITIONER 1, closed.
LMP: Okay. SIGNAL CONDITIONER 1, closed.
CC: Okay. And GLYCOL PUMP 2, closed.
LMP: Okay. I've closed the following circuit breakers, in addition to 13: SIGNAL CONDI- TIONER 1, GLYCOL PUMP 2, TRANSLUNAR BUS TIE, and I've opened the CROSS TIE BALANCE LOADS.
CC: Okay, very good, Ed. What we want to do, now, is put some loads on the LMP BUS for the load test. Now you can go over to panel 16, Ed. And on panel 16, I'd like the - under INSTRUMEN- TATION - the SIGNAL SENSOR, closed.
LMP: Okay. It's closed.
CC: Okay. Under ECS, DISPLAYS, closed.
LMP: ECS DISPLAYS, closed.
CC: And under HEATERS, the RCS SYSTEM A and B, four all heaters - circuit breakers, closed. A/B-2
LMP: Okay. Under HEATERS, RCS SYSTEM QUADS 1, 2, 3, 4 are closed.
CC: Okay, very good. Now back on panel 11 we have AC BUS A and B, BUS TIE INVERTER breakers, all four of them, closed.
CC: Okay. AC BUS A and B, I've closed the four BUS TIE INVERTER breakers.
CC: Okay. Under AC BUS A, the AC BUS VOLTS, closed.
LMP: AC BUS VOLTS, closed.
CC: Okay. Under AC B, the SYSTEM ENGINEER WINDOW HEATER, closed.
LMP: Okay. SE WINDOW HEATER's closed.
CC: And under AC BUS A, the COMMANDER's WINDOW HEATER, closed.
LMP: Okay. COMMANDER's WINDOW HEATER, closed.
CC: Okay, now if you'd scurry back over to the other side under 16, we have EPS INVERTER 2, closed.
LMP: EPS INVERTER 2, closed.
CC: Okay, Ed. Now if you'11 check the AC BUS and turn on INVERTER 2 - turn INVERTER switch to number 2.
LMP: Okay, Joe. And I'm reading right at the high end of the green band. Just under 38 volts indicated.
CC: Okay, very good. Now, turn your MONITOR to BATTERY l, and we'd like the RCS SYSTEM A/B-2 QUAD HEATERS, all four, to the MANUAL position, Ed.
LMP: Okay. They're in MANUAL.
CC: Okay. Now let's bring BATTERY 5 NORMAL switch ON.
LMP: Okay, stand by. BATTERY 5 NORMAL is coming ON.
LMP: And BATTERY 5 seemed to have picked up - picked up about 12 amps indicated.
LMP: And is sharing the load with 1 and 2, apparently.
CC: Okay, looks good. And standby just a few more seconds, Ed.
CC: Okay, Ed. Now let's start bringing - taking the descent batteries off. First of all, we'd like BATTERY 1 to OFF/RESET.
LMP: BATTERY 1, OFF/RESET.
CC: Okay. And let's remain in this configuration for a few seconds here. OFF/RESET.
CC: Okay, Ed, now bring BATTERY 2,
LMP: Okay. BATTERY 2 is OFF, and BAT 5 is carrying the whole load at 30 amps.
CC: Yes. Looks good here.
LMP: Looks good to me.
CC: Okay. Give us about a minute here, Ed, and we'11 press on to the next step.
LMP: Okay. Sure have a good - Moon view out the Commander's window here.
CC: Okay, Ed. We're ready to press on now. Let's turn BATTERY 6 BACK-UP, ON.
LMP: Okay. BATTERY 6 BACK-UP is ON.
CC: Okay. We'11 remain here for a few seconds and take a look at her - -
LMP: ... Okay. 5 and 6 seem to be sharing the load.
CC: Okay, Ed. Now BATTERY 6 BACK UP, OFF.
LMP: Okay. It's OFF.
CC: Very good. Now, let's take BATTERIES i and 2 HI VOLT to ON.
LMP: Okay. i and 2 HI VOLTS are ON. OFF/RESET.
UNKNOWN: Okay. BATTERY 5 NORMAL,
LMP: 5, OFF/RESET.
CC: Okay. Now on the circuit breakers over there, the RCS SYSTEM A/B-2 QUADS, all four breakers, open.
LMP: All four, open.
CC: Okay. You can turn all four heater switches to the OFF position.
LMP: That's completed.
CC: Okay. Now turn the INVERTER switch, OFF.
CC: Okay and INVERTER 2 breaker, open.
CC: Okay, Ed. Now let's finish deactivating here - that wasn't that looks like a good check. Can - on your audio panel, you can turn your T/R, S-BAND OFF.
CC: Okay. And I guess we want to stand by here just a moment, Ed.
CC: What we're doing right now, Ed, is just watching the open circuit voltage on that TM here for a few minutes to make sure it's stable.
LMP: And using up good juice as well.
CC: (Laughter) Yes.
LMP: Houston, 14. Can we press on and get powerdown? We're using juice.
CC: Yes. We're just about ready to press on, Ed. Okay, Ed. We're going now with the intercomms, S-BAND PM, OFF, OFF, OFF.
LMP: Okay. OFF/RESET.
CC: And your RANGING to OFF/
LMP: Okay. You have PM, OFF, OFF, OFF, OFF, RESET.
CC: Okay. And TELEMETRY, OFF, and LO.
LMP: Okay. You have OFF and LO.
CC: Okay, on 16 circuit breakers, Ed. Under EPS, CROSS TIE BALANCE LOADS, open.
LMP: Okay. CROSS TIE BALANCE LOADS are open.
CC: Okay, and you can select low taps on batteries.
LMP: Okay. Low taps on the batteries.
CC: Okay, Ed. Now you can go back to that activa- tion checklist and configure the - both circuit breaker panels as per page 1-3 and 1-4 and I'11 stand by. And if you will, give me a call when you're finished with that.
LMP: Panel 11's configured.
CC: Very good, Ed. Okay, Stu. If you're ready, you can transfer back to CSM power now, and we'11 get the time, if you'11 give us a mark.
LMP: Hold it Just a second. I still haven't got 16 configured yet, Joe.
CC: Oh, okay. Stand by, Stu.
LMP: Okay, Joe; it's completed. Stu's transferring power.
CMP: Okay, Joe. Here it comes back to the CSM. 3, 2, 1 -
CC: Okay, Stu. We've got it. Thank you very much. Okay, Ed, now on your ECS _anel, you can close the DESCENT WATER and OXYGEN.
LMP: Completed.
CC: Okay. CABIN REPRESS closed.
LMP: The CABIN REPRESS is closed.
CC: On panel 11, on your circuit breakers the EPS, DC BUS VOLT, open.
LMP: It's open.
CC: And on panel 16 under ECS, CABIN REPRESS, open.
CC: Okay. You can roll the window shades back up now, Ed.
LMP: Okay. The window shades are going up, and the old Moon is sure getting big in the Commander's - Commander's window at this point.
CC: Okay. Very good. You're not very far from there, on the chart up here, that's for sure. Okay, Ed, on panel 3, FLOODLIGHT, OFF.
LMP: Growing noticeably in the last hour.
CC: Okay. We copy that. And on panel 3 now, FLOODLIGHT, OFF.
CC: Okay, Ed, the CABIN RELIEF and DUMP OVERHEAD to open.
LMP: Verify, it's open.
CC: Okay. Now you can IVT back to the command module, and close the hatch behind you. And we thank you very much.
LMP: Okay. Is everybody satisfied with the checkout, Joe? Are we GO?
CC: Yes. It looks good, Ed.
LMP: Okay. The LM hatch is secured.
CC: Okay. Very good, Ed.
CC: And, Ed, we'11 have some more elaborate words for you on those batteries. The battery 5 holds the load real good. It stands up under the load real good. I think they want to evaluate a few more parameters here, and so far it looks like there's nothing to worry about.
LMP: Okay, Joe. Thank you.
CDR: Houston, 14. Shall we put the hardware back in the tunnel?
CC: Okay. Stand by, Al.
CC: Apollo 14, this is Houston. Roger, Al, you can go ahead, and put the hardware back in and get back into normal configuration.
CMP: Okay. That's in work.
CC: Okay, we'd like POO and ACCEPT, and we'11 pump you up the state vector, preliminary target load and REFSMMAT.
CC: Did you copy, 147
UNKNOWN: We've got it.
CC: 14, Houston. The computer is yours now.
CC: Okay, I have a preliminary LOI maneuver pad ready.
LMP: Okay, Fredo. I'm ready to copy your prelimi- nary LOI-1 pad. SPS/G&N,
CC: Okay, it's 63306, plus 0.90, minus 0.33; 082:36:46.55; minus 2801.9, minus 1105.3, minus 0227.3; 351, 258, 326; 0172.3, plus 0058.4; 3020.6, 6:12, 3013.1; 12, 288.3, 27.1; and the rest of the col_Jmn N/A. Star 15, Sirius, and star 12, Rigel.
CC: Okay, on the zero mark, the set stars R-aline, 127; P-aline, 148; Y-aline, 015; no ullage; LM weight, 33675.
LMP: Fredo, would you give me the minutes of NOUN 33 again, please?
CC: Okay, 36.
LMP: Okay, it's an LOI preliminary SPS/G&N, 63306, plus 0.90, minus 0.33; 082:36:46.55; minus 2801.9, minus 1105.3, minus 0227.3; 351, 258, 326; 0172.3, plus 0058.4; 3020.6, 6:12, 3013.1; 12, 288.3, 27.1; the rest NA. Set stars, Sirius and Rigel, at 127, 148, 015; no Ullage; LM weight, 33675.
CC: Okay, Ed; was good readback.
CDR: And, Houston; 14. Did you get the 93s and the torquing time?
CC: We've got the 93s, Al, but we need the torque time.
CDR: Okay, 079:39:20.
CC: Copy, 079:39:20.
CC: Al, while you still maybe got that pad book handy, I got a TEI-4 pad ready to come up.
CDR: Okay. Go ahead with your pad.
CC: Roger. TEI-4: SPS/G&N; 38242; plus 0.90, minus 0.33; 091:17:38.52; plus 3903.4, plus 0706.3, minus 0165.8; 181, 069, 012. Rest of co21_mn N/A. Ullage four jets, 14 seconds. Other re- marks: assumes burn undocked, and assumes no DOI. Okay and - -
CDR: TEI-4 and SPS/G&N - -
CC: Okay, I've got one correction before you read back, Al. They gave me the docked pitch and yaw trim, the NOUN 48s, and I need to change those on you right now. Okay. The pitch should be minus 0.57, and the yaw trim, plus 0.40.
CDR: Okay, I have it as follows: TEI-4: SPS/G&N, plus 38242; minus 0.57, plus 0.40; 091:17:38.52, plus 3903.4, plus 0706.8. I need DELTA-Vz; 181,069,012; four-jet ullage, 14 seconds, burn undocked.
CC: Okay, Al. NOUN 81, I maybe heard you wrong. DELTA-Vy, first, should be plus 0706.3; and the DELTA-Vz, minus 0165.8, and the last remark is "assumes no ROI."
CDR: All right, will repeat DELTA-Vy, plus 0706.3, and minus 0165.8; last remark, "assumes no _DOI."
CC: Okay, if Ed's got a minute there, I'd like to pro- ceed through a little bit of looking at the high gain.
LMP: Okay, Fredo. Just l, please.
LMP: Okay, I'm ready. What do you want to do?
CC: Okay, first match your dial of pitch and yaw indications with what you're reading on the indicators.
CC: Now, MANUAL and WIDE.
LMP: Okay, you have it.
CC: Okay, put the HIGH GAIN SERVO ELECTRONICS switch back to PRIMARY, and after that go through another normal acquisition.
LMP: 0keydoke.
LMP: It locked up, immediately, Fredo.
LMP: The only thing different than what it was doing this morning was that, it was not increasing sig- nal strength immediately upon going to MEDIUM or NARROW.
LMP: And - and, of course, it seemed to be oscillating after that. It's steady now.
CC: Is everybody on the line now, Al, so I can pass up this docking probe status?
CDR: Houston, can we give you a call in about 20 minutes?
CDR: Houston, 14. I have the null bias check figures for you.
CDR: Okay, we went from minus 100, to minus 985.
CC: Okay, we got that, Al.
CDR: Houston, Apollo 14. We're ready for the discus- sion of the probe, now.
CC: Okay, Al. Okay, the conclusion down here is that on your final attempt, the probe spring started to compress slightly, followed by the capture latch engagement talkbacks going barber pole. The bottle then fired and the retraction looked nor- mai, although the time was somewhat shorter due to the contingent firing of the command module RCS jets. The talkback operation during the initial extension in the final docking, plus the accelerometer data, and also the look-see at the capture latch release motor currents during the extension, all indicated a normal extension, cap- ture, and retract sequence. Some consideration, Al, was given to the possibility that the RCS drogue/probe thrusting compressed the maybe until the docking latches engaged, but the final word was that this would require more force than the RCS could provide. And I guess the most important fact is - as discussed yesterday, we're GO for the mission.
CDR: Okay. Do you suggest any special docking technique for the final docking and rendezvous?
CC: Yes, we're, we're still - -
CDR: I'm thinking of course in - -
CC: Okay, we don't have any - -
CDR: - - I'm thinking, of course, in terms of the different masses.
CC: Roger, Al. We don't have any procedure ready at this time. We're still thinking about the possi- bilities, and we'11 have that ready for you before the time.
CMP: Hey, Fred?
CMP: Okay, could we hit that again, now? I guess I don't understand why - why it didn't work on the other - on the other docking.
CC: Yes, I guess we don't have that answer for you, Stu.
CC: Ail, all we can say is - -
CMP: Are - are we saying that the - -
CC: Yes. We can't explain the preceding attempts, but all we're saying is that the one that worked looked normal.
CMP: Okay, I guess I disagree with it looking normal, but the probe sure does look good now. Are you saying there's no correlation between the retrac- tion and the - I mean, using the retract bottle and getting the docking?
CC: Stand by 1, Stu.
CC: Okay. I'm not sure if I'm answering the question you, you, asked, Stu, but what the data showed is that the - the bottle had fired, and started to pull things in before you all actually worked the switch and maybe you thought the reverse was true.
CMP: What? Let me see - say that again, Fred. I don't understand that one.
CC: Okay, I guess there's a distinction in, maybe your impressions, and what the data said was that you did get captured, normally before the bottle was fired. Did you all have a different impression?
CMP: Yes. Stand by 1.
CMP: Yes, Fred, our impression was that - see the talk- backs going barber pole, which would indicate the capture by the latches - didn't happen until, oh, I think as A1 said the other time, several seconds after he hit the RETRACT switch.
CMP: Hey, but we're not trying to talk you out of anything that - we think the probe is - is - fine, we just want to make sure we're clarified on the procedures.
CC: Okay, Stu.
CC: Okay. We'd like POO and ACCEPT, and we'11 get you in the final vector and target load.
CMP: Okay, Fredo. You got it.
CC: Okay. And I'm ready with the LOI pad now.
LMP: Stand by 1, Fredo.
LMP: Just a minute, Fred. Is this going to be a correction to the previous pad, or a complete new pad?
CC: Well, it's a final one, and I think there's enough difference, you probably ought to use another sheet there.
LMP: Ready to copy. SPS/G&N;
CC: Okay. 63306; plus 0.90, minus 0.33; 082:36:42.70; minus 2804.9, minus 1103.5, minus 0227.0; 351, 258, 326; 0169.3, plus 0058.1; 3022.7, 6:12, 3015.2; 12, 288.3, 27.1. The rest of cold,mu N/A, and all the comments in the set stars information is the same as before. SPS/G&N;
LMP: Okay. On the LOI pad, 63306; plus 0.90, minus 0.33; 082:36:42.70; minus 2804.9, minus 1103.5, minus 0227.0; 351, 258, 326; 0169.3, plus 0058.1; 3022.7, 6:12, 3015.2; 12, 288.3, 27.1; the rest, N/A, and set stars and ullage, and LM weight remain the same.
CC: Good readback, Ed.
CC: And, 14; Houston. The computer's yours.
CDR: Okay, Houston. Good.
CC: Ed, if you have any problem acquiring with the high gain back at LOS - or AOS - in AUTO, just put her in MANUAL and WIDE, and we can get the dump and everything there.
LMP: Okay, Fredo. Will - will do.
CC: 14, Houston. When you can work it in, I got the map updates for REV 1.
CMP: Okay, Fredo. I'm ready to copy.
CC: Okay. LOS, 82:23:58; 180: 82:38:30; AOS with, 82:56:27; and AOS without, 82:49:15.
LMP: Okay, Fredo. 82:23:58; 82:38:30; and the one
CC: Okay. When you get to the - or it's convenient in here, Ed - when you're fiddling with the 02 heater switches, we'd like the 50-WATT HEATER breaker on 226 for tank 3 that you have open, we'd like that one closed now.
LMP: You have it, Fredo.
LMP: Houston, Apollo 14. How do you read now?
LMP: Okay, I am on OMNI Charlie.
CC: Okay, Ed. Copied OMNI Charlie.
CDR: Houston, we're in burn attitude.
CC: Roger. In burn attitude.
CMP: And, Houston; 14. The sextant star check is real good.
CC: 14, Houston. We've got your VGS and P40, and they look mighty fine.
LMP: How you doing today, Ron?
CC: Hey, real good.
CC: Hey, 14; Houston.
CC: Okay, Ed. We're still showing the 02 flow up a little bit for about an hour now. I Just wondered there. You still venting something maybe?
LMP: We turned it off a few minutes ago. It should be coming down shortly.
CMP: It's already started to drop down Fredo. I think it '11 be down normal real soon.
CC: Hey, Al. Everything looks good down here and you have a GO for LOI.
CDR: Thank you. We'11 give it a GO for LOI.
CC: Okay. We're about 45 seconds now to LOS, Ed. We'11 see you on the other side.
LMP: Roger, Fredo. Thank you.
CDR: Okay, Fredo. We had an extremely fine burn, the burn report as follows: burn time, 6 plus 11; residuals, 0.3 plus zero, and zero; DELTA-V c, minus 7.3; 0351; oxidizer, 349.
CC: Okay, 14. We copied. Wonder if you can give us a reading on the unbalance.
CDR: Okay. It was decrease 40, 40.
CC: Roger, Al. Decrease 4 0.
CDR: Roger. This is really a wild place up here.
CMP: Hey, Ron, you're not going to believe this. It looks just like the map.
CC: Hey, that's great, Stu.
CMP: Okay, Fredo; you might tell Ron there that, at this Sun angle, things look real good. Picked up that landmark 1 on the zero phase. Our zero phase tar- get, no sweat, and landmark 2, I got the A part of that one, at least.
CC: Hey, Stu, that sounds great, by golly. It looks like our orbit - orbital science is off to a good start then.
CMP: Yes. For now, anyway. I think we'11 probably get better as time goes on, but it really looks - it really looks great as far as picking up all the targets that we looked at so long.
CDR: Well, this really is a wild place up here. It has all of the grays, browns, whites, dark craters that everybody's talked about before. It's really quite a sight. Ed and Stu are looking at the landmarks to the map, picking up landmarks very easily as we go along the way. And, of course, in the type of orbit we are, the fact that we're climbing away from the surface is very obvious. Of course, that brings more and more of the area in detail. It really is quite a sight. No atmosphere at all; everything is clear up here. Really fantastic.
CC: Roger, Al. We copied, and I think you covered all bets with the colors there.
CC: Al, I expect that you guys - -
CDR: That's because they're all here, Fredo.
CC: Al, I expected you to invent a new one on this flight.
CDR: Give us - give us a little time. We'11 think up something.
CC: l_, Houston.
CC: Go ahead, Fredo.
CC: Ed, can you verify the FLOW VALVE is in INCREASE now?
LMP: That's verified. It's in INCREASE. And I put it in INCREASE about 50 seconds before the end of the burn, and left it there.
LMP: Fredo, the - I think the best description - the description that comes to my mind, we mentioned this when we first looked at this thing, is that it looks like a plaster mold that somebody has dusted with grays and browns, but it looks like it's been molded out of plaster of paris.
CC: Okay. The S-IVB impact should occur in about 8 minutes. We'11 give you the word on that, when it happens. And the first look at trajectory says you're in a 169.6 by 58.9.
CMP: Okay, Fredo. We copy that. And looking out of my rendezvous window now, we've just passed over Sklodowska, and those rays coming out of that bright crater that Ron and I talked about - stand out a lot better than what I expected to see them, Ron.
CC: He's listening.
CDR: Fredo, I copy 168.6 by 56.9. Is that correct?
CC: No. The numbers were 169.6 by 58.9.
CDR: Okay. 169.6, 58.9. Thank you.
CMP: And, Fredo, you might pass on to Ron there, while he's listening, that I was on the wrong side of the cockpit there for old King. I couldn't tell anything about the rays coming down from Bruno. Maybe next time around.
CMP: Okay, we're just now passing over Ansgarius and La Perouse. The cone in Behaim is more rounded, I guess, than what I expected - expected to see. ..., you know, was talking about it being large and quite rounded. It is that - it's a little more subdued than what I expected to see.
CMP: And I can see off to my right here Humboldt coming up, and it's just as impressive as it is in the pictures. One thing that strikes me about it is, the dark areas aren't quite as dark, I guess, as I thought, but we're moving in with a reasonably high Sun here, so they're kind of washing out.
CC: And, 14; Houston. Hate to pull you away from the window, but I got a map update and a flight-plan update when you get a chance.
CC: Okay, on the map update, REV 2, 180 degrees at 84:44:53.
CDR: Okay, I show 084:44:53 for REV 2 on the map.
CC: Roger. That's correct, Al, and in the flight plan at 88: BO -
CC: Okay, change the LTC attitude to roll, 352; pitch, 146; yaw, 355.
CDR: Okay, LTC attitude 88:30, 352, 146, 355.
CC: Okay, and the reason for the big change is the other angles were for SEF and they should be for BEF, and that's what I Just gave you. Next change is at 89:08.
CC: Okay, HIGH GAIN angles should be PITCH, minus 46; YAW, 194.
CDR: Okay, I show minus 46 and 194.
CC: Okay, that's it, Al.
CDR: Thank you, Fredo.
LMP: Fredo, as interesting as this is from orbit, it sure makes one eager to get - to want to get at Cone Crater now. I'11 bet it's wild down there.
CC: Okay, I missed your first there, Ed. What'd you say about Cone Crater?
UNKNOWN: I said, as interesting as this is from orbit, all it does is whet your appetite to get to Cone Crater.
CDR: I guess in 3 days I haven't brainwashed him where the real science is done, Fredo.
CDR: His arms aren't long enough to bring him back from there.
CMP: Okay, you can really get the attitude rate as we're climbing up here to apogee, Houston, and we're climbing right up with Langrenus there.