摘要
FG47固体发动机是CZ2C/FP运载系统轨道转移动力装置,它可以将卫星(如铱星)从椭圆停泊轨道转移到630km圆形运行轨道。该发动机由中国航天工业总公司河西化工机械公司研制,于1997年9月首飞成功,将一个模拟卫星送入轨道。
FG 47 solid rocket motor is the orbit transferring propulsion device for CZ 2C/FP launching system which can transfer the satellite (such as the Iridium Satellite) from the elliptical parking orbit to the 630km circular operating orbit. It was researched and developed by Hexi Chemical Machinary Corp. of CASC and first successfully flighted in Sep 1997 to send a simulated satellite into the orbit.
出处
《固体火箭技术》
EI
CAS
CSCD
1998年第4期4-6,共3页
Journal of Solid Rocket Technology
关键词
轨道转移
固体推进剂
火箭发动机
变轨
Orbit transfer Solid propellant rocket engine Launch vehicle