Results 1 to 10 of about 24,612 (245)

Self-propelled chemotactic ionic liquid droplets [PDF]

open access: yesChemical Communications, 2015
[P6,6,6,14][Cl] droplets show self-propelled movement within open fluidic channels along the liquid–air interface in directions determined by external chemical gradients.
Francis, Wayne   +3 more
openaire   +3 more sources

Attitude and propellant flow control system and method Patent [PDF]

open access: yes, 1962
Attitude and propellant flow control system for liquid propellant rocket ...
Escher, W. J. D.
core   +1 more source

Liquid storage tank venting device for zero gravity environment Patent [PDF]

open access: yes, 1967
Venting device for liquid propellant storage tank using magnetic field to separate liquid and gaseous ...
Graham, R. W., Papell, S. S.
core   +1 more source

Vapor liquid separator Patent [PDF]

open access: yes, 1968
Vapor-liquid separator design with vapor driven pump for separated liquid pumping for application in propellant ...
Ward, W. D.
core   +1 more source

Hot wire liquid level detector for cryogenic fluids Patent [PDF]

open access: yes, 1966
Hot-wire liquid level detector for cryogenic ...
Olsen, W. A., Jr.
core   +1 more source

Autophage engines: towards a throttleable solid motor [PDF]

open access: yes, 2018
This paper describes the instrumented test firing of a rocket that seeks to combine the throttleability of a liquid-fueled engine with the simplicity of a solid motor.
Dron, Mykola   +5 more
core   +1 more source

Tank construction for space vehicles Patent [PDF]

open access: yes, 1967
Liquid propellant tank design with semitoroidal ...
Blumrich, J. F., Loy, C. A.
core   +1 more source

Rocket injector head [PDF]

open access: yes, 1968
A high number of liquid oxygen and gaseous hydrogen orifices per unit area are provided in an injector head designed to give intimate mixing and more thorough combustion.
Green, C. W., Jr.
core   +1 more source

Cryogenic propellant management: Integration of design, performance and operational requirements [PDF]

open access: yes, 1985
The integration of the design features of the Shuttle elements into a cryogenic propellant management system is described. The implementation and verification of the design/operational changes resulting from design deficiencies and/or element ...
Cole, T. W.   +3 more
core   +1 more source

Passive propellant system [PDF]

open access: yes
The system utilizes a spherical tank structure A separated into two equal volume compartments by a flat bulkhead B. Each compartment has four similar gallery channel legs located in the principal vehicle axes, ensuring that bulk propellant will contact ...
Hess, D. A.   +2 more
core   +1 more source

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