Spacelog Gemini 3

Molly Brown, Molly Brown, RKV.

RKV, this is Molly Brown.

Roger. Read you loud and clear. I'm going to update your T_R and transmit a maneuver load to you.

Roger.

I've got a reject on my T_R. What is your status, Molly Brown?

Do you want me to tell them about the oxygen pressure being off-scale?

Our status is GO. We did bring the ECS O₂ back down on the scale with O₂ High Rate, and since that time it has returned to off-scale.

Roger, and I have transmitted a T_R and Gemini load for your maneuver over Corpus. Confirm you were in CATCH-UP. Over.

Negative. We're in CATCH-UP, now.

Roger. I'll retransmit the load.

Roger. You have a load in the CATCH-UP for your maneuver.

Got to be in CATCH-UP.

Okay. There you go.

Roger. Go.

You are GO for the next orbit.

Roger. Thank you.

Are you ready to copy your maneuver times?

Stand by.

Roger.

You ready?

Yes.

Okay. We're ready to copy.

Roger. Your GMTB…correction, 15 57 00. Your ground elapsed time to burn, 01 33 00. Your ΔV of the burn, 048. Your length of burn, 01:14.

Roger. We copied 15:57, 01:33, 48ft/sec, at a minute and 14 seconds.

74 seconds.

Well, 1 minute 14. You want to read it back to them?

Did you get him the other one?

Neg. Wait until I'll get them.

Roger. Stand by for a GET time hack.

On my mark, it'll be 85 minutes and 45 seconds. Stand by.

MARK! You copied?

Roger. We copied.

Roger. Your clocks looked good on the ground.

Will you give me a readout of core 25, 26, and 27? Over.

26 and 27 are all zeros.

I wonder if he got it?

I don't know.

Molly Brown, RKV CAP COM.

Go ahead. Over.

Go ahead RKV.

Will you give me a readout of your computer core — 25, 26, and 27, please?

Roger. It was: 25 was minus 0480. 26 and 27 were all zeros. Over.

That is affirmative. I concur.

Molly Brown, can you give me a readout of your OAMS helium source pressure, temperature, and your propellant quantity gage.

The propellant quantity gage is 83 percent. Stand by. John will give you the other.

Roger. Source pressure is 2450. Source temperature is 85°, and fuel and oxidizer regulated at 295 with 68°.

Propellant quantity is 84 percent.

Roger. I copy.

Molly Brown, RKV standing by. Do you have anything else?