Rocket systems, which are operated either with gel propellants or with hybrid propellant combinations, show combinations of safety and performance benefits which are advantageous in comparison to conventional liquid and solid rocket propulsion systems ...
Naumann, K., Kobald, Mario, Ciezki, H.
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Recent advances in engineering nano/microrobots for tumor treatment. [PDF]
Qin X +7 more
europepmc +1 more source
Recent Developments in Metallic Degradable Micromotors for Biomedical and Environmental Remediation Applications. [PDF]
Dutta S +6 more
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A study on the multidisciplinary design optimization of hybrid-rocket propulsion
Hybrid rocket engines are considered a promising option for reducing the environmental impact of microsatellite launchers. They offer higher safety than solid propulsion systems and better manufacturing conditions compared to liquid propulsion. However, their lower regression rate and combustion efficiency have hindered their widespread adoption.
Matos, Joana +7 more
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Light-driven micro/nanobots. [PDF]
Vardhan RK, Kumar M, Xavier J.
europepmc +1 more source
Simulation Model for Hardware-in-the-Loop Tests of the ILR-33 AMBER Rocket Control System. [PDF]
Cieśliński D +4 more
europepmc +1 more source
Application of Gaussian SVM Flame Detection Model Based on Color and Gradient Features in Engine Test Plume Images. [PDF]
Yan S, Gao Y, Zhang Z, Li Y.
europepmc +1 more source
Metal-Carbon Synergy in C60@Ru Nanocomposite for High-Performance Hydrazine Fuel. [PDF]
Mu X, Wang J, Wang S, Zhang Y, Yang J.
europepmc +1 more source
Modeling fatigue damage evolution in CMDB propellant based on dynamic modulus. [PDF]
Yao L +4 more
europepmc +1 more source
Development of Hybrid Rocket Thrusters for Space-Probe Propulsion
KAMPS, Landon +3 more
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