ANTI-STALL HYDRAULIC PUMP FOR A THRUST VECTOR CONTROL SYSTEM

摘要

A thrust vector control system (100) is provided. The thrust vector control system (100) may comprise an anti-stall hydraulic pump (120) configured to deliver hydraulic fluid to at least one actuator (145, 155), wherein each actuator may be configured to move an exhaust nozzle (5) of a space vehicle (1). The anti-stall hydraulic pump (120) may provide thermal conditioning to the thrust vector actuation control system (100) during ground operation and/or periods of low output operation.