[HTML][HTML] A review on solid propellant micro-thruster array based on MEMS technology

J Xu, J Zhang, F Li, S Liu, Y Ye, R Shen - FirePhysChem, 2023 - Elsevier
With the development of micro-spacecraft technology, micro-nano satellites have the
advantages of small size, low power consumption, short development cycle, formation …

Reaction rate and thermal effects of hydrogen peroxide decomposition in microfluidic chips containing channel-type silver catalysts

Y Yang, Y Ye, P Zhu, W Zhang, R Shen - Catalysis Science & …, 2024 - pubs.rsc.org
As an important application of microfluidic chips, liquid chemical microthrusters need to
introduce a structured catalyst block in the design process. In this paper, a structured silver …

[HTML][HTML] Development of high burn rate propellant and testing in miniature rocket motor for control applications

YR Alexander, N Rathi, PA Ramakrishna - FirePhysChem, 2024 - Elsevier
For aerospace vehicles, notably missiles or satellites for attitude and divert control, impulsive
thrusters are most desirable if they are quantized as exact instantaneous pulses available …