The Test Technology for Thrust Misalgnment Study on Liquid Rocket Engine of Satellite
Tang Jia-peng
Abstract
Tang Jia-peng
Abstract
The thrust vector test of liquid rocket engine on satellite is a high and new technology.Based on the characteristics and measuring requirements of the thrust vector of the liquid rocket engine,the thrust parameter definition is elaborated and then the rotating table test principle and calculation method is introduced in this paper.
A significance statement is not available in the OpenAlex record.
A contribution statement is not available in the OpenAlex record.
Method details are not available in the OpenAlex metadata.
Findings are not separately available in the OpenAlex metadata.
Limitations are not available in the OpenAlex metadata.
Application details are not available in the OpenAlex metadata.
The thrust vector test of liquid rocket engine on satellite is a high and new technology.Based on the characteristics and measuring requirements of the thrust vector of the liquid rocket engine,the thrust parameter definition is elaborated and then the rotating table test principle and calculation method is introduced in this paper.
Key concepts: Thrust, Aerospace engineering, Liquid-propellant rocket, Rocket engine, Satellite, Rocket (weapon), Rocket engine nozzle, Engineering