First attempt of a laser thruster space flight test: Lost at launch

被引:17
作者
Gurin, A., V [1 ,2 ]
Kuvaev, K. Yu [1 ,3 ]
Loktionov, E. Yu [1 ]
Protasov, Yu S. [1 ]
Sirenko, K. N. [1 ]
Zakharov, V., I [1 ]
机构
[1] Bauman Moscow State Tech Univ, Moscow 105005, Russia
[2] Rosatom State Corp Co, NIKIMT Atomstroy, Obninsk Engn Ctr, Obninsk 249030, Russia
[3] Russian Acad Sci, Inst Phys & Technol, Moscow 117218, Russia
基金
俄罗斯基础研究基金会;
关键词
Laser ablation; Laser propulsion; Micro-thruster; Small satellite; Electric propulsion; ORBIT; PLASMA;
D O I
10.1016/j.optlastec.2019.105656
中图分类号
O43 [光学];
学科分类号
070207 ; 0803 ;
摘要
Laser thrusters represent a new class of electric propulsion devices. To the best of our knowledge, Dr. Phipps' mu-thruster prototype (2008) represents the highest technology readiness level to date. So LDU-7 presented in this paper is the world's first laser thruster approved for a space flight. With carbonized PTFE as a fuel irradiated by a 10 W fiber-coupled diode laser, it was rated for 4 mN pulsed (5 ms to CW) thrust and 400 s specific impulse. Fitting within CubeSat 2U dimensions, such thruster is of great interest for small spacecraft due to its comparatively high specific impulse, imparted momentum low bit (1 mu N*s) and wide dynamic range (up to 3 decades). LDU-7 was supposed to rotate hosting satellite 'Baumanets-2' within damping capability of its attitude control system. LDU-7 has been lost with all other payload due to 'Fregat' upper stage failure after launch by 'Soyuz 2.1b' from Vostochny on 28.11.2017. Here we present briefly the description of LDU-7 design and performance, details of its testing program, and planned experiment.
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页数:6
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