摘要
本文对模型－助推火箭并联组合气动设计所涉及的组合体受力状态、纵横向稳定性，以及连接份离等问题进行了探讨与分析，其分析和建议有助于今后开展与并联问题有关的自由飞试验研究。
The probl ems concerning aerodynamic design on model booster parallel connection(including the analyses of force condition of equilibrium,longitudinal/lateral stability and connection/separation) are explored and analysed in this paper.The analyses and suggestions made in this paper arc of important guiding significance for future free-flight test research concerning modelbooster parallel connection.
关键词
模型自由飞试验
助推箭
气动特性
火箭
model free-flight test rocket booster model-booster combiner stability
