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Zero G Liquid Propellant Orientation by Passive Control
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English
Abstract
This paper discusses the advantages and problems associated with the use of “passive” liquid containment systems that utilize liquid intermolecular forces for propellant orientation in reduced or zero gravity environments. Liquid orientation is required to provide reliable engine restart and tank venting operations of space vehicle propulsion systems. Various liquid containment system concepts, and associated design criteria, are presented and general problem areas of interface stability, liquid slosh, and effects of thermal energy are described. Descriptions of present and planned test facilities designed to provide reduced gravity environments and extended time durations are included. It is concluded that additional design criteria in the problem areas discussed must be obtained before “passive” liquid containment systems can replace systems now used in reduced or zero gravity environments.
Authors
Citation
Paynter, H., Mackenzie, C., Marsh, R., and Tyler, V., "Zero G Liquid Propellant Orientation by Passive Control," SAE Technical Paper 640239, 1964, https://doi.org/10.4271/640239.Also In
References
- “Rocket Propellant and Pressurization Systems” Chapter 13 Special Zero Gravity Fluid Problems Englewood Cliffs, N.J. Prentice-Hall, Inc. 1964
- Clodfelter, R. G. “Fluid Mechanics and Tankage Design for Low Gravity Environments.” September 1963
- Reynolds, W. C. “Behavior of Liquids in Free Fall.” J. Aero-Space Sciences December 1959
- Petrash, D. A. Zappa R. F. Otto, E. W. “Experimental Study of the Effects of Weightlessness on the Configuration of Mercury and Alcohol in Spherical Tanks.” NASA April 1962
- Clodfelter R. G. Lewis, R. C. “Fluid Studies in a Zero Gravity Environment.” June 1961
- Petrash, D. A. Nussle R. C. Otto, E. W. “Effect of the Acceleration Disturbances Encountered in the MA-7 Spacecraft on the Liquid-Vapor Interface in a Baffled Tank During Weightlessness.” NASA January 1963
- U.S. Standard Atmosphere 1962 NASA, USAF, U.S. Weather Bureau
- Jacchia, L. G. “Corpuscular Radiation and the Acceleration of Artificial Satellites.” Nature June 13 1959
- Muir, D. E. “A Derivation of the Force Exerted on a Charged Satellite by the Geo-Magnetic Field.” The Martin Co. Denver June 1959
- Johnson F. S. “Satellite Environment Handbook.” Stanford University Press Stanford, Cal. 1961
- Jensen, D. C. Murray R. W. Welch, J. S. Capt. Jr. “Tables of Adiabatic Invariants for the Geo-Magnetic Field” Air Force Special Weapons Center April 1960
- Harkins, W. D. “The Physical Chemistry of Surface Films.” New York Reinhold Publishing Co. 1952
- “Development of Expulsion and Orientation Systems for Advanced Liquid Rocket Propulsion Systems.” April 1963
- Maxwell, J. C. “Capillary Action.” Scientific Papers ii Dover Publications, Inc. 585
- Petrash, D. A. Nelson T. M. Otto, E. W. “Effect of Surface Energy on the Liquid-Vapor Interface Configuration During Weightlessness.” NASA January 1963
- Burnett M. K. Zisman, W. A. “Relation ofWettability by Aqueous Solutions to the Surface of Low-Energy Solids.” J. Phys. Chem. August 1959
- Bauer, H. F. “Propellant Sloshing.” ABMA November 5 1958
- Eulitz, W. R. “Analysis and Control of Liquid Propellant Sloshing During Missile Flight.” NASA, Marshall Space Flight Center December 1961
- Abramson H. N. Ransleben, G. E. “Simulation of Fuel Sloshing Characteristics in Missile Tanks by Use of Small Models.” American Rocket Society Journal July 1960
- Nyland, F. S. “Fluid Slosh Test Program RL 16803 i.” The Martin Co. January 1958
- Usiskind C. M. Siegel, R. “An Experimental Study of Boiling in Reduced and Zero Gravity Fields.” ASME Paper 60-HT-10 August 1960
- Sherley, J. “Nucleate Boiling Heat Transfer Data for LH 2 at Standard and Zero Gravity, Advances in Cryogenic Engineering.” 8 New York Plenum Press
- Adelberg, M. “Gravitational Effect Upon Nucleate Boiling Heat Transfer.” Adv. in Astronautical Sciences 14 1963