NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Surface tensions of propellantsAn apparatus is described for determining the surface tension of propellants by measuring the maximum bubble pressure using two capillaries of different bores. The innovation is the use of a pressure transducer coupled to a bridge supply and a strip chart recorder for registering the development of the pressure difference as the bubble is formed and released. This enables the measurements to be made under controlled atmospheres and to be remotely operated. Preliminary experiments were done on propellant-grade hydrazine and monomethylhydrazine, and on purified hydrazine, at temperatures between 275.4 and 353.2 K. Straight-line expressions and logarithmic expressions reproduce equally well the variation of surface tension with temperature. Contaminated hydrazine, pre-exposed to coupons of 6Al-4V titanium alloy for long periods, gives slightly higher values of surface tension.
Document ID
19720021303
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Razouk, R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 6, 2013
Publication Date
April 1, 1972
Publication Information
Publication: JPL Quarterly Tech. Rev., Vol. 2, No. 1
Subject Category
Propellants
Accession Number
72N28953
Distribution Limits
Public
Copyright
Public Use Permitted.
Document Inquiry

Available Downloads

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