Nitrogen Tetroxide Corrosion Products

Abstract

Study of the phenomenon of flow decay, begun on earlier programs, was continued with a change to MSC PPD-2A propellant (N2O4 + 0.6 percent NO). Flow decay occurs with this propellant, even when dry (less than 0.1-percent water equivalent), as a result of deposits of the solid corrosion product, NOFe(NO3)4. It was found that the presence of excess water in amounts up to the general use limit of 0.2 percent changed the characteristics of the deposits formed when nitrogen tetroxide is heated, then cooled prior to or during flow. Instead of the crystalline solid (NOFe(NO3)4) which is deposited from dry propellant, gelatinous or viscous liquid phases are formed in wet propellant. The appearance of these deposits is governed by an equilibrium solubility limit similar to that observed for the solid deposits in dry propellant. The gelatinous or viscous liquid deposits were not observed to adhere to and plug valves and orifices, as does NOFe(NO3)4, but they did clog filters. Chemical additives previously shown to be effective in dissolving and eliminating NOFe(NO3)4 were not effective against the deposits obtained from wet propellant. Traces of aluminum and titanium were detected in flow decay deposits obtained from flow systems with aluminum and titanium tanks.

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1969
Accession Number
AD0853432

Entities

People

  • E. F. Cain
  • F. C. Gunderloy Jr.
  • J. E. Sinor
  • M. J. Stutsman
  • R. I. Wagner

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Additives (Chemicals)
  • Air Force
  • Aluminum
  • Chemical Synthesis
  • Chemistry
  • Corrosion
  • Dissolving
  • Liquid Phases
  • Materials
  • Metals
  • Phase
  • Phase Separation
  • Propellants
  • Rocket Oxidizers
  • Rocket Propulsion
  • Stainless Steel
  • Valves

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Petroleum Engineering
  • Rocket Propulsion.