OXIDIZER MISCIBILITY STUDIES,

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Abstract:

The three-phase solid-liquid-gas relationship for the binary system nitrogen tetroxide and oxygen was determined over the pressure range of 2.7 psia triple-point pressure of pure N2O4 to 2175 psia. The addition of O2 to N2O4 was found to lower the freezing point of the system 24.7 F. The higher-temperature portion of the S-L-G locus was found to exhibit a minimum temperature of 40 psia and -12.9 F. Author

Author(s):
Hurt, L. J.
Author Organization(s):
ROHM AND HAAS CO HUNTSVILLE AL REDSTONE RESEARCH LABS
Pagination:
0035

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
S-84
Contract/Grant Number(s):
DA-01-021-AMC-11040(Z)
 Subject Terms
Communities of Interest:
No COI(s) Identified
Descriptor(s):
(*OXIDIZERS, ROCKET PROPELLANTS), (*MIXTURES, OXIDIZERS), PHASE STUDIES, FUELS, SOLID ROCKET PROPELLANTS, NITRIC ACID, EXPERIMENTAL DATA, ENTHALPY, LIQUID ROCKET PROPELLANTS, STORAGE, FREEZING, PRESSURE, TEMPERATURE, FEASIBILITY STUDIES, TEST EQUIPMENT, SAMPLING, LIQUEFIED GASES, NITROGEN COMPOUNDS, OXIDES, ENTROPY, CRYOGENICS, SOLVENTS
Field(s)/Group(s):
Rocket Propellants
Keyword(s):
NITRIC ACID INHIBITED RED FUMING
Report Date:
1966 Aug 01