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Improving the Combustion Performance of a Hybrid Rocket Engine using a Novel Fuel Grain with a Nested Helical Structure
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(E)-1,1,4,4-Tetramethyl-2-tetrazene (TMTZ): A Prospective Alternative to Hydrazines in Rocket Propulsion

Anne Dhenain1, Chaza Darwich1, Carlos Miró Sabaté1

  • 1Univ Lyon, Université Claude Bernard Lyon 1, CNRS, CNES, Airbus Safran Launchers, LHCEP, Bât. Raulin, 5thfloor, 2 rue Victor Grignard, 69622, Villeurbanne, France.

Chemistry (Weinheim an Der Bergstrasse, Germany)
|May 13, 2017
PubMed

Keywords:
2-tetrazenesenergetic materialshydrazinesrocket propulsionsynthesis optimization

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