Determination of thermodynamic properties of AeroZINE-50 Final report
Thermodynamic properties of aeroZINE at pressures .001 to 60 psia and temperatures from minus 100 to 250 degrees F
Copeland, J. P.↗
Engineering topics
Simmons, J. A.
Publications and source records attributed to Simmons, J. A..
Reactions and expansion of hypergolic propellants in a vacuum.
Reactions and expansion of hypergolic rocket propellants in vacuum
Fletcher, R. F.↗
Study of propellant valve leakage in a vacuum Final summary report
Adverse effects of liquid propellant leakage past control valves in vacuum environment
Copeland, J. P.↗
Liquid propellant tests in a vacuum chamber Final report, 7 Jun. 1966 - 7 Jun. 1967
Reactivity and expansion characteristics of Aerozine-50 and nitrogen tetroxide from vacuum chamber tests
AEROZINE↗
Determination of thermodynamic properties of AeroZINE-50, phase 1
Literature survey of, and test procedure for determination of thermodynamic properties of AeroZINE-50
Copeland, J. P.↗
Some difficulties of operating liquid systems in a vacuum.
Liquid propulsion systems operating in space and resulting problems of phase transformation, noting plug formation and flow stoppage
Gift, R. D.↗
Study of propellant valve leakage in a vacuum Final report, 7 Jun. 1965 - 15 Aug. 1966
Leakage through propellant valves into injector flow passages and combustion chambers in vacuum
Copeland, J. P.↗
Some difficulties of operating liquid systems in a vacuum.
Liquid propulsion systems operating in space and resulting problems of phase transformation, noting plug formation and flow stoppage
PROPULSION SYSTEM↗
Lunar excursion module propulsion systems valve actuating tests Final report, 7 Apr. - 23 Jul. 1966
Performance of propellant valve actuating system for lunar excursion module descent and ascent engines in vacuum environment
Gift, R. D.↗
Study of propellant valve leakage in a vacuum Phase II report, 14 Jan. - 7 Mar. 1966
Adverse effects of aerozine-50 leakage through propellant valves into injector manifolds exposed to vacuum environment
LEAKAGE↗
Study of propellant valve leakage in a vacuum Phase IV report, 10 Dec. 1965 - 14 Jan. 1966
Propellant evaporative freezing in rocket engine manifolds
FREEZING↗
Study of propellant valve leakage in a vacuum Phase I report, 7 Jun. - 24 Nov. 1965
Propellant valve leakage and propellant flow system freezing and blockage when exposed to vacuum environment in Apollo service module engine
FREEZING↗