Author:
DeLuca L.T.,Galfetti L.,Severini F.,Rossettini L.,Meda L.,Marra G.,D'Andrea B.,Weiser V.,Calabro M.,Vorozhtsov A.B.,Glazunov A.A.,Pavlovets G.J.
Reference17 articles.
1. Theory of Rocket Motors;Alemasov,1980
2. Model of aluminum agglomerate evolution in combustion products of solid rocket propellant;Babuk;Journal of Propulsion and Power,2002
3. Combustion characteristics of aluminum hydride at elevated pressure and temperature;Bazyn;Journal of Propulsion and Power,2004
4. T. Bazyn, R. Eyer, H. Krier, N. Glumac, Dehydrogenation and burning of aluminum hydride at elevated pressures, AIAA Paper 2004-789, 2004
5. M. Calabro, LOX/HTPB/AlH3 hybrid propulsion for launch vehicles boosters, AIAA Paper 2004-3823, 2004
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