Development of Mid‐Way Testing Contingencies for Solid Rocket Motor Processing
Author:
Affiliation:
1. Chemical and Mechanical Testing Labs QC (Process and Labs) Solid Motors Propellant Complex, SDSC-SHAR Sriharikota 524124
Publisher
Wiley
Subject
General Chemical Engineering,General Chemistry
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1002/prep.202200316
Reference11 articles.
1. Rheology of HTPB propellant. I. Effect of solid loading, oxidizer particle size, and aluminum content
2. Effects of Ammonium Perchlorate Particle Size, Ratio, and Total Contents on the Properties of a Composite Solid Propellant
3. A Study on the Improvement of Rheological Characteristics of HTPB/AP Propellant;Park S.;Polymer,2019
4. Oxidizer coarse-to-fine ratio effect on microscale flame structure in a bimodal composite propellant
5. Size and Shape of Ammonium Perchlorate and their Influence on Properties of Composite Propellant
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