1) airframe/scramjet integration
机体/推进一体化
1.
Some performances,such as aerodynamics,aeroheating,radar cross section(RCS),airframe/scramjet integration,and volume of airframe,trimmed characteristic,static stability and maneuverability at cruise stage are selected as the objectives.
采用多目标遗传算法,以飞行器外形参数作为设计变量,考虑了巡航状态下的气动力、热、雷达散射截面、机体/推进一体化、机身容积、配平特性、静稳定性和机动性等指标。
2) Incorporate thruster
一体化推进器
3) airframe/propulsion integrative hypersonic flight vehicle
机体/推进一体化高超声速飞行器
4) promote mechatronics technique
推动机电一体化
5) integrated full electric propulsion(IFEP)
一体化全电力推进
6) airframe-inlet integration
机体/进气道一体化
补充资料：固液混合火箭推进剂(见火箭推进剂)
固液混合火箭推进剂(见火箭推进剂)
solid-liguid hybrid rocket propellant
guye hunhe huoiian tui)in)i固液混合火箭推进剂(s olid一Iiguid hy-brid rocket proPellant)见火箭推讲齐，}_
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条