Gemini 5 Technical Debriefing, Part II, 1965
NASA-UAP-D020 · page 37 of 325
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32 Cooper Conrad Conrad good. Ther e again, it might have been a f unction of the thrusters going out. In any event, I think that 1 s an error ,;hat somebody needs to look i nto. I ' m not sure that pl atfor m mode is doing what i t should. I know that , t heoretically, • and by t he diagrams on it and the limit s that it ought to be a very precise control modE!. Spacecraft separation at SECO + 20 couldn ' t have been better , just fine. Translat i on per igeE! adjust went like cl ockwork. That was our fir st r eal burn and I thi r.k we got something like 9. 6 f t/sec on t he IVI ir.stead of 10 .0, but t he burn wasn ' t that crit icaJ . I checked accelerometer bias and it seE•med like the accel er ometer bias incr eased l at er in the f light . I specif ically checked it f or the REP end it was okay. I 1d just set up zer os in the wirdow and went to Catch-Up and they stayed zero for 3 or 4 minutes or longer . So that satisfied me. I checked it l ater on in the f light and I don ' t think we r an more than a minute and we clickEd up a f oot per second on the fore- aft window. That can be checked on the tape . In the beginning it was entirely acceptable for the REP.