Rocket engine ignition flame reduction system

摘要

A method and apparatus for launching a space vehicle. Operation of a first portion of a plurality of rocket engines associated with a space vehicle is started such that a flow of a gas is initiated through a duct system under the plurality of rocket engines. The gas is located in an area near the plurality of rocket engines. Operation of a second portion of the plurality of rocket engines associated with the space vehicle is started after the flow of the gas begins traveling through the duct system to launch the space vehicle.