- Ken Mattingly
-
That's negative, Jack. We haven't powered up any of the downlink at this time. You'll be doing this and the command module RCS pressurization both by yourself.
- Ken Mattingly
-
Okay. Now, the next event is going to be the separation of the service module, and these are some LM steps, but so that you will know what is going on, I'll read them to you. The LM will do a LM plus-X of one-half foot per second. Then you'll be hitting the CM SM SEP on and up, on their command. As soon as we are free of the service module, the LM will do another LM minus-X for 0.5 feet per second. This is called the push-pull maneuver. I think it was described this afternoon.
- Ken Mattingly
-
Okay. I just wanted you to know that's the sequence you're in. Okay. At the completion of that, we go back to panel 8, and it's SEQUENTIAL, PYRO ARM, both of them, to SAFE.
- Jack Swigert (CMP)
-
Okay. Panel 8: SEQ LOGIC, two, to OFF. Are they ON now, Ken? I don't remember turning them—I guess that's part of one of the other sequences, huh? That we turned them ON?
- Ken Mattingly
-
That's affirm. The reason we're turning the logic off, Jack, is a power savings. So we'll be turning them off, and I'll be getting them back on when we go to get off of the LM; and then turn them back off, then we'll be turning them on prior to entry. Just so you know what's coming.
- Ken Mattingly
-
Okay. Then following this, the LM will pitch up to acquire the Moon—Excuse me, they're going to pitch up and acquire the service module and photograph, and they'll be using the ACA for rotations from now on. And you may see the LM out of window number 5 at the same time they pitch up to acquire it.
- Jack Swigert (CMP)
-
Okay. The LM pitches up, acquires the service module and photographs it, and I should expect to find—might possibly see the service module out of window 5.
- Ken Mattingly
-
That's affirmative. Okay, now we're down to EI minus 3 hours, or the next time-event, and the LM starts a maneuver to what we call the Moon-view attitude. This maneuver is designed to place the command module optics pointing with zero zero at the Moon, and it will be flown to on the LM ball angle.
- Jack Swigert (CMP)
-
Okay, the LM maneuvers to the Moon-viewing attitude which would place the Moon in the center of the command module optics with them at zero zero.
- Ken Mattingly
-
That's affirmative. Okay, now we're going to panel 5, and it's circuit breaker G&N, COMPUTER, MAIN B, closed.
- Ken Mattingly
-
That's affirmative. Now you're going to come up with a 37 ENTER 06 ENTER most likely on the computer. And what we want to do is to put the computer to standby; if you come up with a 37 06, you'll have to do an ENTER in order to get the code 62. If it's got 62 on it, you can do a PROCEED until the DSKY blanks. You might remember that the AC is still off at this time so you won't be getting the STANDBY status light, and your cue that the computer is indeed in standby is when the DSKY goes blank.
- Jack Swigert (CMP)
-
Okay. You're saying that I will probably get a PROGRAM 06 with a VERB 37 ENTER flashing.
- Ken Mattingly
-
Yes. We think that you're going to come up with a 37 06 already in the DSKY. If you do, do an ENTER and that should take you to the code 00062, which is the request for standby. And when you get that, hit PROCEED until the DSKY blanks. If you come up with something else, that's where we want to end up anyhow. With either, when you get the code 62 when it comes up, just do a PROCEED on it.
- Ken Mattingly
-
I don't believe so, Jack. That's one that when you get to that step, if you do get something else, we will be standing by to see that you see. The whole scheme is to go to standby.
- Ken Mattingly
-
Okay. Now, we're at EI minus 2 plus 30; we're going to panel 5: circuit breaker ESSENTIAL INSTRUMENTATION, MAIN A, closed.
- Ken Mattingly
-
Okay, Jack. And that's correct. I got it out of sequence. Would you put that COMPUTER, MAIN A, ahead of LM POWER?
- Jack Swigert (CMP)
-
Okay, Ken. That's CB G&N, COMPUTER, MAIN A, closed, goes before CB LM POWER-1 and -2, open.
- Ken Mattingly
-
That's correct. Jack, what we're doing is we've had the LM powering MAIN B, and we've had all these particular loads on it, and we're getting ready to secure LM power so we wanted to make sure that essential things like the computer, the platform, and all have dioded power supplies before we remove the LM power.
- Ken Mattingly
-
Okay. Thank you. All right, now panel 275: circuit breaker MAIN B, BATTERY BUS B, closed.
- Jack Swigert (CMP)
-
CB INVERTER POWER 1, 2, and 3, closed.
Expand selection up Contract selection down Close - Ken Mattingly
-
That's correct. On panel 5: circuit breaker BATTERY RELAY BUS, BATTERY A and B, closed.
- Ken Mattingly
-
That's correct. Back to panel 5. Circuit breaker EPS SENSOR SIGNAL, AC 1 and 2, closed.
- Ken Mattingly
-
That's correct. On panel 3: AC INVERTER, AC BUS 1 and 2, RESET and back to the center.
- Ken Mattingly
-
And TELCOM, GROUP 2, to AC2.
Expand selection down Contract selection up - Ken Mattingly
-
All right. I assume you got that. Panel 5: circuit breaker IMU, MAIN A and MAIN B, closed.
Spoken on April 17, 1970, 2 a.m. UTC (54 years, 6 months ago). Link to this transcript range is: Tweet