Experimenting on semiconductors using ablative laser propulsion to investigate propulsion parameters

被引:3
|
作者
Abbas, Ayesha [1 ]
Zakaria, Muhammad Qaiser [1 ,2 ]
Iqbal, Syeda Tehreem [3 ]
Jamil, Yasir [1 ]
机构
[1] Univ Agr Faisalabad, Dept Phys, Faisalabad 37000, Pakistan
[2] Univ Lahore, Dept Phys, Sargodha Campus, Sargodha 40100, Pakistan
[3] Univ Lahore, Dept Phys, Lahore 54000, Pakistan
关键词
laser ablation propulsion; silicon; microthruster; momentum coupling coefficient; specific impulse; cavity aspect ratio; space debris; SPACE DEBRIS; POLYMERS; REMOVAL;
D O I
10.2351/7.0000965
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
A laser can be used to propel distant objects. The ability of silicon to produce thrust and its propulsive parameters are needed to be studied in ablative laser propulsion (ALP). In this work, pure silicon and silicon doped with indium were subjected to ALP to achieve the momentum coupling coefficient and specific impulse to investigate its worth as a propellant. The experiment was conducted using the Nd:YAG laser (Quantel Brilliant) operating at fundamental harmonic (? = 1064 nm and 5 ns pulse duration). In the given range of fluence, 1 x 10(5)-5 x 10(5) J/m(2), no significant difference among both samples for values of momentum coupling coefficient (C-m) and specific impulse (I-sp) is observed; for instance, both propellants follow a decreasing trend for C-m. However, maximum enhancement for C-m and I-sp is observed with a cavity aspect ratio of one. C-m and I-sp are enhanced about 1.75 and 4.5 times, respectively, for pure silicon. The external cavity does not have any impact on C-m values for indium-doped silicon while values of I-sp showed considerable enhancement.
引用
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页数:8
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