achlp600 : Solid Propellants Specific Impulse
About
Add a short description of your repository
Wiki
Source
B. P. Mason, C. M. Roland. Solid Propellants // Rubber chemistry and technology, Vol. 92, No. 1, pp. 1–24 (2019) https://doi.org/10.5254/rct.19.80456
Source Abstract
Solid propellants are energetic materials used to launch and propel rockets and missiles. Although their history dates to the use of black powder more than two millennia ago, greater performance demands and the need for‘‘insensitive munitions’’ that are resistant to accidental ignition have driven much research and development over the past half-century. The focus of this review is the material aspects of propellants, rather than their performance, with an emphasis on the polymers that serve as binders for oxidizer particles and as fuel for composite propellants. The prevalent modern binders are discussed along with a discussion of the limitations of state-of-the-art modeling of composite motors.
Repository Details
Fig-4.png describes specific impulse vs binder content for solid propellants employing HTPB with ammonium nitrate (AN), ammonium perchlorate (AP), ammonium dinitramide (ADN), and an ammonium dinitramide formulation bound with glycidyl azide polymer (GAP). This is an adapted data from L. T. DeLuca, Eurasian Chem. Technol. J. 18, 181 (2016).
Source
B. P. Mason, C. M. Roland. Solid Propellants // Rubber chemistry and technology, Vol. 92, No. 1, pp. 1–24 (2019) https://doi.org/10.5254/rct.19.80456
Source Abstract
Solid propellants are energetic materials used to launch and propel rockets and missiles. Although their history dates to the use of black powder more than two millennia ago, greater performance demands and the need for‘‘insensitive munitions’’ that are resistant to accidental ignition have driven much research and development over the past half-century. The focus of this review is the material aspects of propellants, rather than their performance, with an emphasis on the polymers that serve as binders for oxidizer particles and as fuel for composite propellants. The prevalent modern binders are discussed along with a discussion of the limitations of state-of-the-art modeling of composite motors.
Repository Details
Fig-4.png describes specific impulse vs binder content for solid propellants employing HTPB with ammonium nitrate (AN), ammonium perchlorate (AP), ammonium dinitramide (ADN), and an ammonium dinitramide formulation bound with glycidyl azide polymer (GAP). This is an adapted data from L. T. DeLuca, Eurasian Chem. Technol. J. 18, 181 (2016).
