Gemini 5 Technical Debriefing, Part I, 1965
NASA-UAP-D019 · page 98 of 223
Text
This text came with the file. It may have mistakes. When the text and the image disagree, the image is right.
93 Conrad Cooper .,,... Conrad Cooper Conrad Cooper ·GONftf1 21 .1 feet per second Delta P. Oh, that was our pre-burn stuff. At 2 days 17 hours 34 minutes and 31 seconds we had a maneuver load. Well , I have the whole thing here. We powered up the platform on day 2 at 15:50 with the plat form caged BEF, and at 16:15 we alined BEF with the rate gyros on. At 16:45:00 the computer went on and we addressed 25 90201 , and apogee adjust maneuver was at 16:50:17. We translated forward to zero the IVI, so it was actually a retro burn. I mean we were BEF. We were using the aft-firing thrusters. Yes. We had a D-6 on the ship , and we didn't see it, at 2 days 16 hours 56 minutes and 49 seconds . We didn't see the ship. Then at 17:20 the second day we alined the platform SEF and we sat the computer up to address 25 00158. We made an SEF burn, which was a phase adjust maneuver, at 17: 34:58 . Now, that one we did in the Platform Mode and it didn't burn for schmaltz. The platform didn ' t hold it . It allowed us to get a little bit of left-right and up- down.