TEI BURN CHART TEI TRIM X AND Z AXIS TO 0.2 FPS BT +2 SEC & ∆VC = -40 FPS ±10° TAKEOVER 10°/SEC TAKEOVER RESIDUALS SHUTDOWN TIME ATT DEVIATION P OR Y RATES 3-100a TRAJECTORY 3292.7 - 1436.0 1436.0 - 1207.0 1207.0 - 0 0 - 90 90 - 100 100 - 149 LUNAR ORBIT UNSTABLE UNSTABLE/ HYPERBOLIC MODE III - AFTER 1 REV MODE II - 2 SPS BURNS FOR ORBIT STABILIZATION AND WATER OR CLA LANDING. MODE I - 1 BURN AT TEI +2HRS P37 AT SPHERE OF INFLUENCE HYPERBOLIC (∆V 580 TO 0, BT 125-149) LOI1 VGO ABORT MODE BT