DSC and TGA Investigation on Ammonium Nitrate-Based Solid Propellant Doped with Ammonium Dichromate for Gas Generator Applications
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Publisher
Springer Nature Singapore
Link
https://link.springer.com/content/pdf/10.1007/978-981-19-1388-4_6
Reference10 articles.
1. Jos J, Mathew S (2017) Ammonium nitrate as an eco-friendly oxidizer for composite solid propellants: promises and challenges. Crit Rev Solid State Mater Sci 42(6):470–498. https://doi.org/10.1080/10408436.2016.1244642
2. Sutton ES, Vriesen CW (1979) Gas generator propellants for aerospace applications. AIAA Paper. https://doi.org/10.2514/6.1979-1325
3. Oommen C, Jain SR (1999) Ammonium nitrate: a promising rocket propellant oxidizer. J Hazard Mater 67(3):253–281. https://doi.org/10.1016/S0304-3894(99)00039-4
4. Kohga M, Nishino S (2009) Burning characteristics of ammonium nitrate-based composite propellants supplemented with ammonium dichromate. Propellants Explos Pyrotech 34(4):340–346. https://doi.org/10.1002/prep.200800060
5. Kumar P, Kumar M, Lakra R (2018) Effect of catalysts on the burning rate of phase stabilized ammonium nitrate based composite propellants. IOP Conf Ser Mater Sci Eng 455(1). https://doi.org/10.1088/1757-899X/455/1/012022
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