Gemini 7 Technical Debriefing, 1965
NASA-UAP-D021 · page 77 of 222
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67 The regul at ed pressure stayed at 300, r ight on the money, throughout the ent ire flight until the auxiliary tank was actuated. We ot:>erated the auxiliary tank when the nressure dr opped about 30 psi . Lovel l Yes . It went down to about 260 or 270. IlonnAn Right. It crune right back up , and the system worked just exactly as advertised. The prope1.1ant ouantity gauge worked fine. Por most of the flight it was right in ae-reement with the ground comt:>utations. Love] J 1:/hat wa.s the final pro"9elJant quantity reading? Borman About 2 percent to 3 percent. Lovell And we still had 300 psi r egulated pressure. Borman Source pressure remained about 1,000 psi. Monitoring of OAMS propellant remaining: On board infomat ion I thought . was good. The OAMS propellant quantity gauge, worked fine . Lovell At least it was on the s i de favoring us . :Sorman Yes. The ground in.formation was excellent. At the end of every da,y they gave us ground r undown of how much O.AMS fuel we had remaining. It worked out fine. We were short on O.&MS fuel. Any time we di dn't have a s~ecific assi gnment, we were in drif t ing f l ight. That's one thing we want men tioned. Every time we powered down we' d turn off the ACME bias power and the ACME inverter, and invariably t hi s would