Gemini 5 Technical Debriefing, Part I, 1965
NASA-UAP-D019 · page 106 of 223
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101 CONFIDENT~ Conrad Then I have Plat form to ORB Rate, Prelaunch, and horizon scan for some r eason. ~uestar 01 , 90 degrees left. Cooper We alined SEF at 13:10. Conrad Oh, that was these platform tests 1 and 2 that they wanted us to do . Cooper That's right. We were getting ready for another stateside pass, too. We installed the photometer, we did an S-8/D-13 pass at day 3, 13 hours 32 minutes at Laredo . Conrad Oh, let me make a comment right now on S- 8/D- 13. We were supposed to make a measurement, a window survey, of the window before day one and the last day. Okay, the window scan was done on 1 day 18 hours 26 minutes 00 seconds. That was the first window scan. A second window scan was never done because the last 3 days of the flight we were in drifting flight . This required a 30- degree sun angle on the window, and we never did have a control system back until we were on the RCS system. We weren' t about to do any experiments on RCS fuel . That was right before retro . The second window scan, the one at the end of the flight , wasn ' t done. But