摘要
织女一号气象火箭是一种小型无控固体火箭,由于采用了若干先进的技术,使其总体性能达到了国际先进水平。本文介绍了其总体性能,重点介绍了总体方案设计中采用的包括最优推力程序等若干先进技术。
The ZN-1 Meteorological Rocket is designed in need of development of
space technology. The overall performances of rocket have reached the adva-
nced world level by means of using some advanced technology. This paper
centers on some advanced technology adopted in the overall design, such as
optimal thrust program.
出处
《国防科技大学学报》
EI
CAS
CSCD
北大核心
1989年第3期16-25,共10页
Journal of National University of Defense Technology
关键词
气象火箭
固体火箭
设计
Moteorological rocket
solid rocket, optimal thrust program, a end buring grain
