NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Vapor flow into a capillary propellant-acquisition deviceAn analytical model is described that specifies the conditions needed to cause a flow of vapor through the screens of a start basket. The analytical model is composed of several original submodels that interrelate the evaporation of the liquid in the basket, the bubble-point change of a screen in the presence of wicking, the drying out of a screen through a combination of evaporation and pressure difference, the vapor flow rate across a wet screen as a function of pressure difference, and the effect on wicking of a difference between the static pressure of the liquid reservoir and the vapor surrounding the screen. Most of the interrelations were demonstrated by a series of separate-effects tests, which were also used to determine certain empirical constants. The equations of the model were solved numerically for typical start basket designs. A simplified start basket was constructed and tested to verify these predictions, using both volatile and non-volatile liquids. The test results verified the trends predicted by the model.
Document ID
19830055153
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dodge, F. T.
(Southwest Research Inst. San Antonio, TX, United States)
Bowles, E. B.
(Southwest Research Institute San Antonio, TX, United States)
Date Acquired
August 11, 2013
Publication Date
June 1, 1983
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 83-1380
Report Number: AIAA PAPER 83-1380
Accession Number
83A36371
Funding Number(s)
CONTRACT_GRANT: NAS3-22664
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available