Aluminum agglomeration reduction in a composite propellant using tailored Al/PTFE particles

By T. Sippel, Steven F. Son, L. Groven. 2014

337 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Materials Chemistry, Mechanics of Materials

View Paper: https://www.semanticscholar.org/paper/62583ee8059d2ea5c268ed669427768dbeeea2b2

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. E. Dreizin
2. S. K. Valluri
3. M. Schoenitz
4. A. Rogachev
5. A. Mukasyan

In Materials Chemistry

1. E. Dreizin
2. S. K. Valluri
3. M. Schoenitz

In Mechanics of Materials

1. E. Dreizin
2. M. Schoenitz
3. S. K. Valluri
4. A. Rogachev
5. A. Mukasyan

Citations in the corpus

• Fluorine-containing oxidizers for metal fuels in energetic formulations (2019, methodology): “70wt% of Al were favored [80,81] as the objective was to maximize the aluminum content enabling reaction with other oxidizers.”
• Study of aluminum particle combustion in solid propellant plumes using digital in-line holography and imaging pyrometry (2017, positive): “The size, velocity and temperature of these metal particulates are important quantities needed to inform combustion modeling [2] and to evaluate new propellant formulations [3, 4].”