摘要
摘要CZ-2C是适用于发射低轨道、质量较大卫星的二级液体运载火箭。本文简述了CZ-2C的由来;阐述了箭上各系统的组成、功能和性能;并以发射返回式卫星和搭载瑞典卫星为例,较详细地给出了CZ-2C的总体性能和飞行程序参数;对可能的轨道分配器设计方案也作了简单说明。
CZ-2C is a two-stage liquid propellant launch vehicle, which is suitable for launching heavier LEO satellite. The paper introduces the evolution of CZ—2C, the subsystems——their schemes, functions and performance, and provides a group of parameters in detail about the overall performance and flight program launching a recoverable satellite and a Sweden piggyback satellite as an example. The design concepts of orbit dispenser have been simply analyzed.
出处
《导弹与航天运载技术》
1993年第3期1-13,共13页
Missiles and Space Vehicles
关键词
运载火箭
系统设计
中国
Launch vehicle
System design
China
