Analysis of Combustion Characteristics of HTPB, Graphite, Aluminum, Iron, and Gaseous Oxygen-Based Hybrid Rocket Propellant
Author:
Publisher
Springer Science and Business Media LLC
Subject
Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering
Link
https://link.springer.com/content/pdf/10.1007/s42405-023-00636-x.pdf
Reference18 articles.
1. Yu H, Yu X, Chen S, Zhang W, DeLuca LT, Shen R (2021) The catalysis effects of acetylacetone complexes on polymer matrix of HTPB-based fuels. FirePhysChem 1(4):205–211. https://doi.org/10.1016/j.fpc.2021.11.009
2. Srivastava S, Thakur AK (2022) Comparison of propellant characteristics using paraffin and blends of aluminum and magnesium with oxidizers in hybrid rocket engine. Aerosp Syst 6:119–128. https://doi.org/10.1007/s42401-022-00175-5
3. Pal Y, Mahottamananda SN, Palateerdham SK, Subha S, Ingenito A (2021) Review on the regression rate-improvement techniques and mechanical performance of hybrid rocket fuels. FirePhysChem 1(4):272–282. https://doi.org/10.1016/j.fpc.2021.11.016
4. Srivastava S, Ingenito A, Andriani R (2019) Numerical and experimental study of a 230 N paraffin/N2O hybrid rocket. In: EUCASS 2019–8th European conference for aeronautics and space sciences, p 1–13. https://doi.org/10.13009/EUCASS2019-866
5. Srivastava S, Thakur AK (2022) Review on hybrid rocket engine: past, present and future scenario. Int Jo Veh Struct Syst 14(5):680–685. https://doi.org/10.4273/ijvss.14.5.24
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