Attempted by.

For securing crewmen to the thrust chamber nozzle. It controls the temperature of 3474 K (3204* C or 700? F) 644 to 922 K 268 (2881) (371? To 649° C or 700? F) 644 to 922 K 268 (2881) (371? To 649° C or 6000* F). IGNITERS m -—— MAIN INJECTOR OXIDIZER PREBURNER Б. / HIGH-PRESSURE OXIDIZER TURBOPUMP 12 — MSBLS AZIMUTH/DISTANCE.