This run is for testing the J246 Launch Vehicle simulation/integrator/rate/rotational simulation/integrator/rate/translational simulation/integrator/position/rotational simulation/integrator/position/translational simulation/notify-time-trigger forces/hold-down simulation/sim-time-sec ge 10000.05 position/h-agl-ft 0.0 0.80 5000.0 0.90 10000.0 1.00 15000.0 0.90 20000.0 0.70 25000.0 0.80 30000.0 0.90 35000.0 1.00 40000.0 1.10 45000.0 1.20 50000.0 1.30 55000.0 1.40 60000.0 1.30 65000.0 1.20 70000.0 1.30 100000.0 1.40 200000.0 1.50 position/h-agl-ft 0.0 10.0 5000.0 40.0 10000.0 60.0 15000.0 120.0 20000.0 135.0 25000.0 140.0 30000.0 130.0 35000.0 120.0 40000.0 110.0 45000.0 110.0 50000.0 100.0 55000.0 90.0 60000.0 85.0 65000.0 60.0 70000.0 40.0 100000.0 10.0 200000.0 5.0 simulation/sim-time-sec ge 6.0 simulation/sim-time-sec ge 12.0 forces/fbx-prop-lbs gt inertia/weight-lbs Output message at 10 second intervals Vehicle state: guidance/executive/MET velocities/eci-velocity-mag-fps guidance/executive/apoapsis guidance/executive/periapsis guidance/executive/eccentricity position/h-agl-ft aero/alpha-deg guidance/executive/gravity-turn-pitch-rate-command velocities/thetadot-rad_sec attitude/phi-rad attitude/theta-rad attitude/psi-rad forces/hold-down fcs/throttle-cmd-norm[0] guidance/executive/current-mode simulation/sim-time-sec >= simulation/notify-time-trigger guidance/executive/left-srb-sep-flag eq 1 guidance/executive/right-srb-sep-flag eq 1 guidance/executive/las-jettison-flag eq 1 guidance/upper-stage-flight-flag eq 1 guidance/upper-stage-flight-flag eq 1 2.0