On data inputs from engine sensors; control.

13, 1977, Free Flight 5 — NOZZLE TUBE 6 — MAIN COMBUSTION CHAMBER FUEL TURBOPUMP М OXIDIZER O 9 PREBURNER N FUEL PREBURNER 9 — HOT-GAS MANIFOLD HIGH-PRESSURE OXIDIZER TURBOPUMP 13 - MAIN OXIDIZER VALVE 14 — MSBLS AZIMUTH/DISTANCE MEASURING EQUIPMENT STATION RUNWAY 15 14 — OXIDIZER PREBURNER VALVE.