Gemini 5 Technical Debriefing, Part II, 1965
NASA-UAP-D020 · page 203 of 325
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192 Conrad Cooper Conrad Cooper Conrad C:et<tfilf)Et◄l l.._4 That's right . You get an idea of how much fuel you use because Ring B was tested but never used until below 65 ,000 feet; we shot 80 percent of the fuel out of it on the drogue. So , it iB no surprise to me that Ring A ran out of fuel . There is no doubt about it that Ring A ua.s still running, unless somebody shows me otherwise on a traces , at least past drogue deploy. It was run ning until at l east we got Ring B running. I really firmly believe, based on what we tried on here and my feeling on the thing, you could shoot two or three orbits of attitude control and align ment and the whole smear of r e ~rofire ar.d the whole reentry and everything on one rin€' with no problem at all . Now, let's look at another thing. When you are at drogue deploy, we were on rate command and there was a high frequency, low amplitude oscillation, but it was well outside the r ate band. So, those thrusters went to steady-state firing. Yes, they did . They were firing full blower all the way, trying to damp. And they did. They did an excellent