A Study on Consumption and Characterization of Stabilizer Content of NEPE Propellant via FTIR
Author:
Affiliation:
1. School of Aerospace EngineeringBeijing Institute of Technology Beijing 100081 P.R. China
Publisher
Wiley
Subject
General Chemical Engineering,General Chemistry
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1002/prep.201800340
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3. D. Zhou X. Liu X. Sui Z. Wei N. Wang Effect of pre-strain during ageing on the maximum elongation of composite solid propellants and its modelling Polym Test.2016 50 200–207.
4. W. Ao P. Liu W. Yang Agglomerates smoke oxide particles and carbon inclusions in condensed combustion products of an aluminized GAP-based propellant Acta Astronaut.2016 129 147–153.
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