#F02K9/46

PRE-COMBUSTION CHAMBER FOR FEEDING A TURBINE IN A LIQUID PROPELLANT ROCKET ENGINE

The pre-combustion chamber for feeding a turbine in a liquid propellant rocket engine, providing energy for driving the fuel and oxidant pumps, according to the invention is a detonation chamber (1) i…

DRIVE·Jan 21·2 min read

F02K9/46 SIEC BADAWCZA LUKASIEWICZ INST LOTNICTWA [PL]

MULTI-TIME IGNITION STARTING APPARATUS FOR A ROCKET ENGINE, AND ROCKET ENGINE HAVING SAME

The present invention relates to the field of space propulsion technology, and in particular, to a multi-time ignition starting apparatus for a rocket engine and a rocket engine having the same. The m…

DRIVE·May 22·2 min read

F02K9/46 BEIJING INTERSTELLAR GLORY TECH LLC [CN]

Conveyor device for cryogenic liquids

The aggregate has a liquid-conveying piston pump provided for liquid gases, and a connector (11) provided in proximity of a lower dead center (12) of movement of a piston (3). The connector is releasa…

DRIVE·Jun 19·1 min read

F02K9/46 ASTRIUM GMBH [DE]

ROCKET ENGINE SYSTEM FOR REALIZING HIGH-SPEED RESPONSE

Disclosed is a turbo pump in which a pump impeller is connected to one end of a rotary shaft and a turbine is connected to the other end of the rotary shaft. The turbo pump is designed such that an eq…

DRIVE·Jul 18·1 min read

F02K9/46 IHI CORP [JP]