#B64G1/402

DIAPHRAGM FOR A FLUID STORAGE TANK

A diaphragm (101) for use in a fluid storage tank in which the fluid storage tank comprises first and second shell portions defining an interior tank space, wherein the diaphragm is configured to be s…

DRIVE·Jul 2·1 min read

B64G1/402 CAM LOCK LTD [GB]

PRESSURIZATION DEVICE FOR ROCKET PROPELLED BY LIQUID OXYGEN AND METHANE AND ROCKET PROPELLED BY LIQUID OXYGEN AND METHANE

The present invention relates to the field of liquid rocket technology, and in particular, to a pressurization device for a rocket propelled by liquid oxygen and methane and a rocket propelled by liqu…

DRIVE·May 29·1 min read

B64G1/402 BEIJING INTERSTELLAR GLORY TECH LLC [CN]

AIRCRAFT/SPACECRAFT FLUID COOLING SYSTEM AND AIRCRAFT/SPACECRAFT FLUID COOLING DEVICE

Provided are an aircraft/spacecraft fluid cooling system and an aircraft/spacecraft fluid cooling method in which a fluid in a pipe installed in aircraft or spacecraft can be cooled efficiently so tha…

DRIVE·Feb 5·1 min read

B64G1/402 MITSUBISHI HEAVY IND LTD [JP]

Demisable fuel supply system

A demisable fuel supply system for a satellite includes a pressurized aluminum alloy tank (12) with an aluminum alloy propellant management device therein. The propellant management device (PMD) can h…

DRIVE·Oct 2·1 min read

B64G1/402 KEYSTONE ENGINEERING COMPANY [US]

Demisable fuel supply system

A demisable fuel supply system (10) for a satellite includes a pressurized aluminum alloy tank (12) with an aluminum alloy propellant management device (20,22) therein. The propellant management devic…

DRIVE·Sep 26·1 min read

B64G1/402 HAMILTON SUNDSTRAND CORP [US]

Augmentation of a monopropellant propulsion system

The system has an auxiliary tank (140) that is in direct contact with a main tank (10) through a pressurizing circuit (14) such that gas i.e. inert gas, in the auxiliary tank is continuously released …

DRIVE·Jul 4·1 min read

B64G1/402 CENTRE NAT ETD SPATIALES [FR]

Liquid propellant tank and vapor jet emitting device including same

A liquid propellant tank (2) for storing a liquid propellant A and supplying vapor produced by evaporation of part of the liquid propellant A to an external location comprises a tank body (21) for sto…

DRIVE·Sep 21·2 min read

B64G1/402 JAPAN AEROSPACE EXPLORATION [JP]

Attenuation element for a fuel supply line system of a spacecraft propulsion system

The system (10) has a cylinder-shaped housing (11) comprising a retaining area (22) that is coupled with a pipeline of a fuel supply-line system (21). An elastic body (12) is arranged in the area and …

DRIVE·Jun 8·1 min read

B64G1/402 ASTRIUM GMBH [DE]