Flow characteristics of orifices for venting launch vehicle compartments
Flow characteristics of orifices for venting launch vehicle compartments
Ramsey, P. E.↗
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Experimental simulation of two-phase venting to a space environment.
Simulation of two phase hydrogen venting to space environment, discussing thrust effect measurements, flow instabilities and instrumentation
Evans, E. A.↗
Analytical study of two-phase impingement for orbital cryogenic venting.
Impingement pressure analysis associated with two phase cryogenic propellant venting to space environment
Evans, E. A.↗
A vented high-voltage system for satellite applications
Vented high-voltage system for power supply of photomultiplier tube in OAO
Laffert, D.↗
Venting vapor apparatus Patent
Fuel tank pressure-relief device for venting cryogenic liquid vapors through tubes with porous plug
Weber, R. J.↗
Characteristics of Fluid Vented into a Vacuum Annual Report
Characteristics of fluid vented into vacuum
Maples, D.↗
Liquid storage tank venting device for zero gravity environment Patent
Venting device for liquid propellant storage tank using magnetic field to separate liquid and gaseous phases
Graham, R. W.↗
Analysis of two-phase impingement from a cryogen vented in orbit
Impingement pressure analysis associated with two phase cryogenic propellant venting to space environment
Evans, E. A.↗
Pressure sensing control development for pressurization and venting systems Final report, 2 Jul. 1969 - 2 Aug. 1970
Hybird electronic controller developed for pressurization and venting systems of space propulsion system
Tobloski, J.↗
Venting device for pressurized space suit helmet Patent
Venting device for pressurized space suit helmet to eliminate vomit expelled by crewmen
Gran, A. A.↗
Space shuttle compartment venting Final report
In-flight venting of space shuttle vehicles investigated using delta wing booster and high crossrange orbiter vehicles as configurations
Haukohl, J.↗
Compartment venting - Space vehicle design criteria
Analysis of internal and external gas venting system of spacecraft
Source record↗
Study of thermal conductivity requirements. Volume 3: Analytical and experimental heat transfer study of a venting cryogen tank
Analysis of heat transfer characteristics of venting cryogen tank - Vol. 3
O'Neill, M. J.↗
UO2 venting and redistribution
Out-of-pile experiment for measuring uranium dioxide fuel redistribution rates, determining vent hole plugging time and thermal cycling
Phillips, W. M.↗
Design curve for liquid helium cryostats with vapor-cooled vent tubes
Design curve for estimating conduction heat transfer liquid He cryostats with vapor-cooled vent tubes
Dicarlo, J. A.↗
Saturn S-IVB continuous vent system for propellant control during parking orbit
Saturn S-4B continuous vent system for propellant tanks during parking orbit to prevent excessive pressure, requiring liquid settling with auxiliary ullaging rockets
Neher, R. T.↗
Design considerations for an orbital nonpropulsive vent system
Orbital nonpropulsive vent system to remove excess or residual propellant vapors and waste gases with minimum impulse imbalances imparted to vehicle
Buchmann, H. F.↗
Fill and vent quick disconnect
Hydraulic disconnect coupling on ground serving half of spacecraft refrigeration cooling system employs movable center stem for venting and closing nipple poppet. Self sealing poppet quickly connects cooling system to spacecraft without manual work. Recessed sealing surface insures open poppet when stem retracts.
Boerner, R. Y.↗