Propulsion system for flying machine, particularly for a missile
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United States of America Patent
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Oct 27, 2015
Issued Date -
N/A
app pub date -
Sep 8, 2011
filing date -
Sep 10, 2010
priority date (Note) -
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Abstract
A propulsion system including: a booster; a turbojet engine; the booster including a chamber which is fixed to a rear casing of the turbojet engine by being arranged along the longitudinal axis thereof, which chamber includes at a rear a jet pipe and includes at least one charge and a mechanism initiating the charge; and gas bleed tubes connected to the booster and which are configured either for igniting the combustion chamber of the turbojet engine on for starting the turbine of the turbojet.
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