GAS LAWS HELP FIND PROPELLANT MASS AT ZERO G
Propellant mass measurement in a rocket fuel tank at any time during zero gravity conditions
ROCKET PROPELLANT TANK↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Saturn monthly progress report /january 16, 1964 - february 16, 1964/
Saturn I, IB, and V launch vehicle progress - second stage launching, static test failure, fabrication progress, and fuel tank hydrostatic pressure test
SECOND STAGE↗
A propellant slosh measuring system for space vehicles
Capacitance sensors for measuring liquid propellant sloshing in space vehicle fuel tanks
SLOSHING↗
Automatic fluid separator supplies own driving power
Centrifugal separator suspended in the fuel tank of a space vehicle selects and vents gas vapor at zero gravity. Escaping vapor is used to drive an expander turbine that is magnetically coupled to the separator.
Decker, M. S.↗
Special tool seals conductors with combination of plastic sleeves
Special tool seals electrical conductors connecting instrumentation within space vehicle cryogenic fuel tanks and oxidizer tanks. An inner sleeve of fluorinated ethylene-propylene and an outer sleeve of tetrafluoroethylene enclose a bundle of conductors and are heated with the tool to form a tight seal of the bundle and each individual wire.
Young, S.↗
The Dynamic Behavior of Liquids in Moving Containers, with Applications to Space Vehicle Technology
Dynamic behavior of liquids in moving containers with applications to propellants in space vehicle fuel tanks
LIQUID SLOSHING↗
Photographic investigation of liquid behavior on temperature and liquid-vapor sensors used in low-gravity environment
Simulated coasting flight test on sensing tip of liquid-vapor sensor for liquid hydrogen fuel tank
LIQUID-VAPOR INTERFACE↗
Manufacturing feasibility study of advanced tankage for recoverable boosters Final report
Manufacturing feasibility of multicell fuel tanks for recoverable lifting body booster
Source record↗
Diffusion bonding of titanium to simulate S-1C fuel tankage components
Developing fabrication methods for diffusion bonding of titanium alloys to meet SIC fuel tank design criteria
Irvine, C. N.↗
Fixed insulation development program Final report
Improved Centaur fixed fuel tank insulation
Source record↗
Reduced gravity liquid configuration simulator
Reduced gravity liquid configuration simulator to study propellant behavior in rocket fuel tanks
Olsen, W. A., Jr.↗
Venting vapor apparatus Patent
Fuel tank pressure-relief device for venting cryogenic liquid vapors through tubes with porous plug
Weber, R. J.↗
Densitometer Patent
Measuring density of single and two-phase cryogenic fluids in rocket fuel tanks
Jacobs, R. B.↗
Techniques for insulating cryogenic fuel containers Patent
Carbon dioxide purge systems to prevent condensation in spaces between cryogenic fuel tanks and hypersonic vehicle skin
Jackson, L. R.↗
Helium in NASA projects now and in the future
Helium properties and utilization in NASA projects, discussing pressurization of fuel tanks cooling of superconducting magnets
Brown, G. V.↗
Low temperature uses of helium at NASA
Helium low temperature applications to fuel tank pressurization, superconducting magnet cooling and cryopumping of solar space simulators
Brown, G. V.↗
Zero gravity separator Patent
Describing apparatus for separating gas from cryogenic liquid under zero gravity and for venting gas from fuel tank
Pope, A. M.↗
Flexible ring slosh damping baffle Patent
Flexible ring slosh damping baffle for spacecraft fuel tank
Brooks, G. W.↗