Sub-scale experimental test of Hybrid Rocket engine using LOX and 3D printed fuel
Author:
Affiliation:
1. Indian Institute of Space Science and Technology Department of Aerospace Engineering
2. Vikram Sarabhai Space Centre
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-3108
Reference15 articles.
1. Okninski,A.,Kopacz,W.,Kaniewski,D.,andSobczak,K."HybridRocketPropulsiontechnologyforspacetransportation revisited - propellant solutions and challenges," Vol. FirePhysChem, KeAi Publishing, No.1, 2021, pp.260-271. https: //doi.org/doi.org/10.1016/j.fpc.2021.11.015,URLhttps://doi.org/10.1016/j.fpc.2021.11.015.
2. Stanley,M."Space: InvestingintheFinalFrontier,"2020. URLwww.morganstanley.com/ideas/investing-in-space.
3. Casalino, L., and Pastrone, D. "Optimal design of hybrid rocket motors for microgravity platforms," Vol.24, Journal of PropulsionandPower,No.3,2008,pp.491-498.
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