Gemini 4 Experiment Debriefing, 1967
NASA-UAP-D018 · page 128 of 224
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Point of Application AV SECO +30 5 5 Beginning of 3rd Rev (3:33) 5 99 min. later (5:12) 4th Rev 12.5 76 min . later (6:28) 5th Rev 21 106 min: later (8:14) 6th Rev 12 l,5th or 16th Re] 30th Rev 25-30 45th Rev 62nd Rev +llO (or 66th Rev~':) NOMINAL GT-4 TRANSLATIONAL MANEUVERS HP/HA After Maneuvers 86/153 88/154 82/153 86/150 93/150 Direction of Thrust Posigrade Retrograde Posigrade Retrograde Posigrade Posigrade ·1 I ! -1 ,5 days 1"': Lifetime Adjustments ~·: For Pacific landing + If available Translational Thruster Aft Aft Fwd Aft Various Aft } Various Aft will be minimum requiried Purpose SIC-Booster Separation Station-Keep on Booster S/C - Separation Rendezvous Maneuver (Start intercept Terminal Phase/Braking Orbital Lifetime Adjust *~'rAdjust lifetime - 4 days Adjust lifetime - 3 days Adjust lifetime - 2 days Achieve OAMS Retrofire