摘要
飞马座空间运载火箭的推进系统为三级固体推进剂火箭发动机,本文对发动机的设计、制造和试验作了全面介绍,重点讨论了三级发动机的设计特点,即为了提高系统可靠性和降低生产成本,采用大的设计安全系数和在其它型号上使用过的成熟技术。
The propulsion system for the Pegasus air-launched space booster consists of three stage solid propellant rocket motors.The design,manufacture and tests of the motors are comprehensively presented,with emphasis on their design feature that a large safe fac- tor in design and demonstrated technologies are used for the system reliability improvement and cost reduction.
出处
《固体火箭技术》
EI
CAS
CSCD
1993年第1期20-24,共5页
Journal of Solid Rocket Technology
关键词
火箭发动机
复合材料
壳体
绝热层
Solid rocket engine
Composite case
Insulation
Nozzle
Pegasus air-launched space booster
