摘要
给出了悬摆法测量激光推进冲量耦合系数的原理，分别以空气、氩气、氮气和氮气为推进剂，用悬摆法测量了抛物形推力器在能量不同的单脉冲TEACO2激光辐照下的冲量耦合系数。实验结果表明：氩气的冲量耦合系数最高，氦气的冲量耦合系数最低；在实验测试的激光能量范围内，4种推进剂气体的激光推进冲量耦合系数基本上都随着激光能量的增加而线性增大，冲量耦合系数的相对误差为5．4％～6．4％。实验结果与国外相关实验结论一致。
The principle to measure the impulse coupling coefficients of laser propulsion with a pendulum system was provided. The impulse coupling coefficients of a parabol laser propulsion thruster were measured with a pendulum system using air, He, N2 or Ar as propellant respectively. The experimental results indicated that the coupling coefficient of the laser propulsion was the highest when the propellant was Ar and it was the lowest when the propellant was He. The relative error of the impulse coupling coefficient was 5.4%-6.4%.
出处
《强激光与粒子束》
EI
CAS
CSCD
北大核心
2006年第2期197-200,共4页
High Power Laser and Particle Beams
基金
国家安全重大基础研究项目
关键词
激光推进
冲量耦合系数
相对误差
悬摆
Laser propulsion
Impulse coupling coefficient
Relative error
Pendulum
