Ignition and combustion characteristics of compound of magnesium and boron

Author:

Liu Lin-lin,Liu Pei-jin,He Guo-qiang

Publisher

Springer Science and Business Media LLC

Reference18 articles.

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2. Gany A, Timnat YM. Advantages and drawbacks of boron-fueled propulsion. Acta Astronaut. 1993;29(3):181–7. doi: 10.1016/0094-5765(93)90047-Z .

3. Besser HL, Strecker R. Overview of boron ducted rocket development. 1993;2(1–6):133–78. doi: 10.1615/IntJEnergeticMaterialsChemProp.v2.i1-6.60 .

4. Buchner E, Langel G. Elementary boron as a propellant component in ducted rockets—thermodynamic study. Z Flugwiss. 1976;24(5):275–8.

5. L-l Liu, G-q He, Y-h Wang. Thermal reaction characteristics of the boron used in the fuel-rich propellant. J Therm Anal Calorim. 2013;114(3):1057–68.

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