Impacts of laser pulse width and target thickness on laser micro-propulsion performance
Authors:
- 1 August 2022
- journal article
- research article
- Published by IOP Publishing in Plasma Science and Technology
- Vol. 24 (10) , 105504
Abstract
In order to optimize the laser ablation performance of a micro-thruster with 1U dimensions, which employs a micro semiconductor laser, the impacts of pulse width and glycidyl azide polymer (GAP) thickness on thrust performance were researched. The results showed that with a GAP thickness of 200 μm, the single-pulse impulse (I) increased gradually with the increase in the laser pulse width from 50 to 800 μs, while the specific impulse (I sp), impulse coupling coefficient (C m) and ablation efficiency (η) all reached optimal values with a 200 μs pulse width. It is worth noting that the optimal pulse width is identical to the ignition delay time. Both C m and η peaked with a pulse width of 200 μs, reaching 242.22 μN W−1 and 35.4%, respectively. With the increase in GAP thickness, I and C m increased gradually. GAP of different thicknesses corresponded to different optimal laser pulse widths. Under a certain laser pulse width, the optimal GAP thickness should be the most vertical thickness of the ablation pit, and the various propulsion performance parameters at this time were also optimal. With the current laser parameters, the optimal GAP thickness was approximately 150 μm, I sp was approximately 322.22 s, and η was approximately 34.94%.Keywords
Funding Information
- National Natural Science Foundation of China (No. 11502301)
This publication has 29 references indexed in Scilit:
- A magnetic coupling thrust stand for microthrust measurementsMeasurement Science and Technology, 2015
- A 10 nN resolution thrust-stand for micro-propulsion devicesReview of Scientific Instruments, 2015
- Sub-micro-Newton resolution thrust balanceReview of Scientific Instruments, 2015
- Research on applications of rectangular beam in micro laser propulsionApplied Surface Science, 2014
- Numerical Analysis of Interaction Between Single-Pulse Laser-Induced Plasma and Bow Shock in a Supersonic FlowPlasma Science and Technology, 2012
- Laser Propulsion Technology on “KKS-1” MicrosatelliteThe Review of Laser Engineering, 2011
- Influence of Pulse Steepness on Vacuum Flashover of Casting Epoxy ResinPlasma Science and Technology, 2009
- Polymer ablation: From fundamentals of polymer design to laser plasma thrusterApplied Surface Science, 2007
- Micropropulsion Using a Laser Ablation JetJournal of Propulsion and Power, 2004
- Micropropulsion using laser ablationApplied Physics A, 2004