Processes during the hypergolic ignition between monomethylhydrazine (MMH) and dinitrogen tetroxide (N2O4) in rocket engines

Research output: Contribution to journalArticleResearchpeer review

Authors

  • Irmgard Frank
  • Anton Hammerl
  • Thomas M. Klapötke
  • Christel Nonnenberg
  • Helmut Zewen

External Research Organisations

  • Ludwig-Maximilians-Universität München (LMU)
  • Airbus Group
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Details

Original languageEnglish
Pages (from-to)44-52
Number of pages9
JournalPropellants, Explosives, Pyrotechnics
Volume30
Issue number1
Publication statusPublished - 24 Feb 2005
Externally publishedYes

Abstract

Two potential sources for engine complications with methylhydrazine/ nitrogen tetroxide rocket engines were examined. The products formed during a cold pre-reaction before the actual ignition of the rocket engine and their later behavior were investigated with Car-Parrinello molecular dynamics simulations. It was found that methyldiazene is the main product of the cold pre-reaction. As a side product, especially in the presence of an excess of methylhydrazine, dimethyltetrazanes are formed. These may be responsible for violent side reactions. We also examined possible plume deposits, which are mainly formed in pulsed mode operation, for their influence upon the operation of a rocket engine. We synthesized methylhydrazinium and dimethylhydrazinium nitrate as well as methylhydrazinium azide and determined their crystal structure and sensitivity.

Keywords

    Fuel, High-Energy Materials, Monomethylhydrazine (MMH), Nitrogen Tetroxide (NO), Rocket Propulsion

ASJC Scopus subject areas

Cite this

Processes during the hypergolic ignition between monomethylhydrazine (MMH) and dinitrogen tetroxide (N2O4) in rocket engines. / Frank, Irmgard; Hammerl, Anton; Klapötke, Thomas M. et al.
In: Propellants, Explosives, Pyrotechnics, Vol. 30, No. 1, 24.02.2005, p. 44-52.

Research output: Contribution to journalArticleResearchpeer review

Frank I, Hammerl A, Klapötke TM, Nonnenberg C, Zewen H. Processes during the hypergolic ignition between monomethylhydrazine (MMH) and dinitrogen tetroxide (N2O4) in rocket engines. Propellants, Explosives, Pyrotechnics. 2005 Feb 24;30(1):44-52. doi: 10.1002/prep.200400084
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