摘要
采用标准试验发动机实测结果及理论计算,研究了HTPB/HMX推进剂比冲与发动机工作压强之间的关系.研究结果表明,在发动机相同的工作条件下,工作压强由5MPa提高到10MPa可使推进齐比冲净增102N.s/kg,发动机工作压强最好选取大于6MPa。这一结果为发动机设计提供了参考依据。
he relationship between the specific impulse of HTPB/HMX propellant and the operating pressure of the motor is studied based on the results from a stanard test motor and the theoretical calculations.The results show that a specific impulse gain of 102 N.s/kg can be obtained in the same motor condition by increasing the operating pressure from 5MPa to 10MPa.The operating pressure of more than 6MPa is preferred which can be used as a reference basis for motor design.
出处
《固体火箭技术》
EI
CAS
CSCD
1995年第1期30-34,共5页
Journal of Solid Rocket Technology
关键词
固体推进剂
火箭发动机
端羟基
聚丁二烯
推进剂
Tarms Solid propellant rocket engine Hydroxy terminated polybutadicne propellant HMX Energetic property