Study to determine an improved method for Apollo propellant system decontamination and propellant tank drying, phase I Interim report
Improve method for Apollo propellant system decontamination and propellant tank drying
APOLLO PROJECT↗
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Results for “TANKS”
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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Projectile-impact-induced fracture of liquid-filled, filament-reinforced plastic or aluminum tanks
Projectile-impact-induced fracture of liquid filled, filament-reinforced plastic or aluminum tanks
FRACTURE↗
Liners for non-metallic tanks Final report
Low temperature elongation of polymide films for nonmetallic-tank liners for liquid hydrogen
LINER↗
An analytical study of liquid outflow from cylindrical tanks during weightlessness Final report
Liquid outflow from cylindrical tanks during weightlessness
CYLINDRICAL TANK↗
The center vent shape for venting a tank in a low gravity environment
Center vent tube effect on zero gravity equilibrium configuration for Centaur launch vehicle, second stage liquid propellant tank ullage
WEIGHTLESSNESS↗
Centaur tank corrosion tests and X-rays
Metal corrosion prevention methods for Centaur launch vehicle liquid propellant tanks
LIQUID PROPELLANT↗
Moment of inertia and damping of liquids in baffled cylindrical tanks Technical report no. 11
Moment of inertia and damping in baffled and nonbaffled cylindrical tanks
MOMENT↗
Effective moment of inertia and velocity ratio for liquid-filled cylindrical tanks oscillating about the longitudinal axis
Effective inertia moment and velocity ratio for liquid-filled cylindrical tanks oscillating about longitudinal axis
OSCILLATING CYLINDER↗
Transfer function analysis of a fluid contained in a longitudinally excited thin-wall cylindrical tank
Transfer function analysis of fluid contained in longitudinally excited thin-wall cylindrical tank
THIN WALL↗
Comparison of propellant sloshing parameters obtained from model and full-size Centaur liquid-oxygen tanks
Comparison of propellant sloshing and pendulum analogy parameters from Centaur liquid-oxygen tanks
LIQUID OXYGEN /LOX/↗
Research and development for fabricating a simulated titanium alloy Y-ring segment for the S-IC fuel tank Phase I and II REPORT, 30 Jun. 1965 - 11 Feb. 1966
Design and processing development, and tooling and fabrication plan for S-IC fuel tank Y-ring segment
TITANIUM ALLOY↗
A Survey of Ring Baffle Damping in Cylindrical Tanks
Survey of Miles method for determination of damping by ring baffles in cylindrical tanks
DAMPING↗
Bubble behavior in liquids contained in vertically vibrated tanks.
Violent bubble behavior in liquids contained in vertically vibrated tanks caused by water hammer type of resonance
BUBBLE↗
Analysis of flexible baffles for damping tank sloshing.
Damping of liquid oscillations in cylindrical tanks, determining rigid and flexible baffle loss coefficients, baffle efficiency and maximum bending stress
LIQUID SLOSHING↗
Bubble behavior in liquids contained in vertically vibrated tanks.
Violent bubble behavior in liquids contained in vertically vibrated tanks caused by water hammer type of resonance
PROPELLANT TANK↗
Experimental investigation of liquid sloshing in a scale-model Centaur liquid-hydrogen tank
Liquid sloshing in scale model Centaur liquid hydrogen tank
ROCKET PROPELLANT TANK↗
Cryogenic liquid experiments in orbit. Volume II - Bubble mechanics, boiling heat transfer, and propellant tank venting in a zero-gravity environment
Bubble mechanics, boiling heat transfer, and propellant tank venting in zero gravity environment - storage and handling of cryogenic liquid propellants in orbit
PROPELLANT TANK↗
Research study for determination of liquid surface profile in a cryogenic tank during gas injection Quarterly progress report no. 9, Jun. 18 - Sep. 17, 1966
Determining liquid surface profiles in cryogenic tank during gas injection
GAS INJECTION↗