首页> 外文会议>International Conference on AEROTECH >Torsional thrust stand for characterization of microthrusters
【24h】

Torsional thrust stand for characterization of microthrusters

机译:扭转推力代表用于微观售票的表征

获取原文

摘要

This paper describes the setup of a precise thrust stand based on torsional pendulum design for characterizing the performance of microthrusters. Calibration has been carried out by using an improved version of electrostatic calibrator, which produces a wide range of accurate and repeatable calibration force. After the calibration, the thrust stand can resolve constant force from 40uN to 3.4mN and impulse bit from 7uNs to 340μNs. The usefulness of the thrust stand has been demonstrated by measuring the performance of two different microthrusters: a pulsed plasma thruster that produces impulse bit of 23.15μNs and a vaporizing liquid microthruster that produces steady state thrust of 633.5μN.
机译:本文介绍了基于扭转摆型设计的精确推力架的设置,用于表征微型助剂性能。通过使用改进的静电校准器进行校准,这产生了各种精确和可重复的校准力。校准后,推力支架可以将恒定力从40U升至34mn和7UN的脉冲钻头到340μns。通过测量两种不同微型杀剂的性能来证明推力支架的有用性:一种脉冲等离子体推进器,其产生23.15μns的脉冲位和蒸发液体微生物,产生633.5μN的稳态推力。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号