Spacelog Apollo 8

Good show. Thank you.

Apollo 8, Houston.

Go ahead, Houston.

we would like to take control of the DSE for a while, Bill.

Go ahead.

Thank you.

Apollo 8, Houston. We would like to get an approximate GET of your SEP maneuver to use for our ephemeris tracking data.

Roger. It was 3 hours 40 minutes zero seconds.

Good, 03:40 and a foot and a half—feet per second. Right?

Roger. About that —

Okay.

— We have the—Mike, we have the exact callout here for you and a burn status report.

Alright.

Alright, DELTA-V_X minus 00011, DELTA-V_Y plus 0002, DELTA-V_Z minus 0002, roll 0, pitch 180, yaw 0. Over.

Roger, Apollo 8.

Apollo 8, Houston.

Go ahead, Houston. Apollo 8.

Roger. At your convenience, would you please go P00 and ACCEPT? We're going to update to your W matrix. And also when you get a chance, we would like to know about the SLA panels. Did they all depart? And do you have any comments about the SLA?

They all departed, and they worked fine.

Okay. Thank you.

We are in P00 and ACCEPT.

Thank you.

Houston, Apollo 8. Will you give us the information when you want us to stop the venting and so on?

Apollo 8. Houston.

Go ahead, Houston.

Roger. What is the venting information are you inquiring about: the O₂ flow high out through the waste tank or waste compartment, or are you talking about your evaporator?

Evaporator. We are configuring now to stop boiling.

Okay.

We concur in that.

Apollo 8, Houston. You can go back to BLOCK. We have gotten in the load to the W matrix update.

Roger.

Houston, Apollo 8. The back pressure valve is closed, and the water flow is OFF.

Back pressure valve closed, and water flow OFF. Thank you.

Houston, Apollo 8 here.

Apollo 8, Houston. Go ahead.

Roger. It looks like I might have to do a couple more small maneuvers to stay away from the front of this S-IVB, the way we are ending up now. Do you want me to do these with our P47 if we have to do them?

Standby one, Frank.

That's affirmative, Frank, on this P47.

Okay. And give me the time again when it starts to dump, please.

Roger. We're working on an exact GET of that, Frank.

Roger.

Apollo 8, Houston.

Go ahead.

I'd like to give you some idea about your trajectory. It looks like a midcourse correction number 1, projected out to TLI plus 6 hours, would be only 7 feet per second. So, of course, any further maneuvers you do would add to that, which is probably good.

I just want to stay from away from in front of this thing.

Roger. We concur. Looks like it is chasing you, huh?

Yes.

OMNI D.

That is the nonpropulsive vent, but it's pretty spectacular. It's spewing out from all sides like a huge water sprinkler.

Roger. Get some pictures of it.

We are.

Say again that big vent time, so I can write it down please, Houston.

Roger. Big vent time 05:07:55, and it will start maneuvering to vent attitude beginning at 04:44:55. Bill has got the tape recorder back.

Thank you. Roger.

We're receiving VHF music now, Houston. Thank you.

Yes, you took the words right out of my mouth, Frank, and we would like to know also how far away from the S-IVB you are now.

I guess we are between 500 to 1000 feet.

Roger.

Herb Alpert seems pretty good.

Houston, Apollo 8.

Apollo 8, Houston.

Roger. I believe we are going to have to vent or thrust away from this thing; we seem to be getting closer.

Roger. Understand, Frank; go ahead whenever—just give us some idea of when you did it and how much.

Roger.

Apollo 8, Houston. Could you stand by one? We are working on something here.

Apollo 8, Houston.

Apollo 8, this is Houston. Over.

Apollo 8, this is Houston. Over.

You are loud and clear, Mike. Go ahead.

Okay, Frank. On your additional separation maneuver, we recommend that you make a radial burn, point your plus X-axis toward the earth, and thrust minus X for 3 feet per second. Over.

I don't want to do that; I'll lose sight of the S-IVB.

Okay. The reason we want a radial burn is to increase your midcourse correction so we can use the SPS. Stand by on it.

Apollo 8, Houston.

Go ahead.

How close to a radial burn can you get without losing sight of the S-IVB, Frank?

Well, I don't know because I can't see the earth now, Mike.

Okay.

We can pitch down some. Jim has the earth in the optics so we could pitch some and get pretty close to one, I guess.

Apollo 8, Houston.

Go ahead, Houston. Apollo 8.

We can give you a pitch gimbal angle on radial direction if that would be a help. It's 181 degrees; pitch gimbal angle would be exactly radial at 4 hours and 10 minutes. I don't know whether that solves your visibility problem or not.

181?

That's affirmative.

Well, then zero would be just as good, wouldn't it?

Frank, if you use zero, then make the SEP if possible in the plus X thrusters. That's the direction of the burn we'd like.

Well, can't do that. I'll thrust right square into that S-IVB.

Yes, okay. Understand.

What will he maneuver to as far as the gimbal angle for his blowdown?

Apollo 8, Houston. At blowdown, that S-IVB should be oriented to perform a retrograde blowdown along the local horizontal.

Okay.

Is it still chasing? Does it look like it is closing on you, Frank?