International Journal of Energetic Materials and Chemical Propulsion

Купить выпуск $198.00 Том 9, 2010 Выпуск 4

DOI: 10.1615/IntJEnergeticMaterialsChemProp.v9.i4

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RADIATIVE IGNITION OF SOLID PROPELLANTS: A PRACTICAL APPROACH
Franck Cauty, Yves Fabignon, Charles Erades
pages 285-304
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v9.i4.10

$45.00

RECENT ADVANCES IN HYBRID PROPULSION
Brian Cantwell, Arif Karabeyoglu, David Altman
pages 305-326
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v9.i4.20

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HIGH-FIDELITY PREDICTIONS OF THE EFFECTS OF PRESSURE AND PARTICLE SIZE ON AMMONIUM PERCHLORATE/HYDROXY- TERMINATED-POLYBUTADIENE PROPELLANTS
Matthew L. Gross, Ephraim B. Washburn, Merrill W. Beckstead
pages 327-339
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v9.i4.30

$35.00

DETONATION CHARACTERISTICS OF NITROMETHANE DILUTED WITH NONEXPLOSIVE LIQUIDS
Sergey Alekseevich Koldunov, Alexander Victorovich Ananin
pages 341-350
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v9.i4.40

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CHARACTERIZATION AND COMPARISON OF TWO HYDROXYL-TERMINATED POLYETHER PREPOLYMERS
Rodrigo I. Caro, John M. Bellerby
pages 351-364
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v9.i4.50

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REDUCTIVE DEBENZYLATION OF 2,4,6,8,10,12-HEXAAZAISQWURTZITANE
Sergey V. Sysolyatin, Alexander I. Kalashnikov, Valeriy Malykhin, Irina A. Surmacheva, Gennady V. Sakovich
pages 365-375
DOI: 10.1615/IntJEnergeticMaterialsChemProp.v9.i4.60