Propulsion
CH-01- LOX tank pressure
- 3.42
- RP-1 tank pressure
- 3.11
- Chamber temp
- 288
- Turbopump RPM
- 32 480
- Helium reserve
- 61 %
- Purge line
- NOMINAL
Twelve stations report to Flight. A single NO-GO stops the count at the next hold point; a HOLD may be cleared by the responsible discipline before T−00:10:00.
| Station | Call | Constraint | Margin | Last update |
|---|---|---|---|---|
| PROP Propulsion | GO | Tank press ≥ 3.05 bar | +0.37 | 04:11:52 |
| GNC Guidance & Control | GO | IMU drift ≤ 0.020 | +0.006 | 04:10:31 |
| ECOM Electrical & Comms | GO | Link margin ≥ 6 dB | +3.4 | 04:05:09 |
| WX Weather | HOLD | Shear < 0.006 s⁻¹ | −0.001 | 04:06:14 |
| RANGE Range Safety | GO | Corridor clear | — | 03:51:40 |
| RCVY Recovery | GO | Sea state ≤ 3.0 m | +0.9 | 03:58:22 |
| THRM Thermal | GO | Skin ΔT ≤ 12 K | +5.1 | 04:09:03 |
| GSE Ground Support | NO-GO | Umbilical retract ≤ 1.4 s | −0.3 | 04:12:01 |
| PAYL Payload | GO | Battery ≥ 88 % | +4 | 04:02:47 |
| FSW Flight Software | GO | Build 4.19.2 verified | — | 01:20:00 |
| MED Pad Medical | GO | Crew on station | — | 03:40:15 |
| PA Public Affairs | GO | Feed uplink live | — | 04:00:00 |
GSE reports umbilical retract 0.3 s over spec. Flight has called a built-in hold at T−00:10:00 pending a second actuation test.
Each event carries an owner, an abort criterion and a recycle path. Nothing on this list is advisory.
White room team clears the tower. Cabin leak check runs for nine minutes against a 0.02 psi/min criterion. A failed check recycles to T−01:10:00 with a 42-minute window remaining.
Clock stops. Weather takes a fresh sounding, GSE reruns the umbilical actuation, and the flight director reconciles any open constraint. This hold absorbs schedule risk without costing window.
All twelve stations report on the loop in fixed order. Flight calls the count. From this point the vehicle transitions to internal power and the ground crew has no path back to the pad.
Ground control hands the count to the vehicle. Human intervention is reduced to a single abort command. Tank pressurisation ramps to flight levels and the flight termination system arms.
Final verbal release. Strongback retracts to sixty degrees, water deluge floods the flame trench, and the pad transitions to unattended state.
Nine engines light in a staggered 300 ms pattern. The vehicle holds down until all chambers report above 92 % of rated thrust; anything short triggers a pad-safe shutdown before release.
Observer credentials grant read-only access to the Meridian flight loop and the archived telemetry wall for LS-092. Credentials expire ninety minutes after landing.