The development of structural adhesive systems suitable for use with liquid oxygen /LOX/ Summary report, 20 Jun. 1969 - 19 Apr. 1970
Development of structural adhesive systems suitable for use with liquid oxygen
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Development of structural adhesive systems suitable for use with liquid oxygen
Saturn V launch vehicle fire and explosion hazard due to S- II insulation tank containing liquid oxygen /LOX/ mixtures
Gas-tungsten arc welding for positioning and inside-locking of liquid oxygen /LOX/ tunnel of Saturn V booster
Injector evaluation in 2400-pound-thrust rocket engine using liquid oxygen and liquid ammonia
Gaseous hydrogen and liquid oxygen experiments in uncooled 20,000-pound-thrust rocket engines
Principle of a vertical falling film is used to clean contaminated large diameter and length liquid oxygen /LOX/ cylindrical ducting. The cleaning cycle is performed by flowing trichloroethylene in a falling film down a vertically mounted duct for approximately one hour.
RP-1 rocket fuel liquid oxygen and liquid hydrogen-liquid oxygen combination explosion hazard
Addition of liquid fluorine to liquid oxygen in Vanguard first stage oxygen-hydrocarbon rocket engine
Comparison of propellant sloshing and pendulum analogy parameters from Centaur liquid-oxygen tanks
Attenuation of tangent-pressure oscillation in liquid-oxygen-heptane rocket engine combustion chamber using longitudinal fin
Heat transfer drag coefficient for ethanol drops in rocket chamber burning ethanol and liquid oxygen
Lubrication characteristics of bearing steel in liquid oxygen in rocket engines
Bulk density of boiling liquid oxygen
Positron annihilation in condensed gases - helium, hydrogen, nitrogen, & oxygen
Liquid nitrogen dilution effect on LOX impact sensitivity
Liquid oxygen set behavior during combustion instability in gaseous hydrogen fueled rocket combustor
Impact sensitivity of foam insulation in presence of liquid oxygen