Design and simulation of the accumulator for servomechanisms of launch vehicle

Design and simulation of the accumulator for servomechanisms of launch vehicle

The accumulator is a crucial component of the hydraulic power for servomechanisms of the launch vehicle, which has a significant effect on the performance and the mass power. Traditional design methods are mostly based on empirical formulas, which do not meet the requirements of the fine design of a...

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Bibliographic Details
Main Authors: Bo Zheng, Chun Zhao, Xin Liu, Shoujun Zhao, Xiaosha Zhang
Format: Article
Language:English
Published: Wiley 2020-10-01
Series:The Journal of Engineering
Subjects:
servomechanisms
vehicle dynamics
design engineering
aerospace control
aerospace simulation
space vehicles
accumulator
hydraulic power
empirical formulas
fine design
aerospace products
physical model
mathematical model
joint simulation model
extreme flight operation profiles
discharge volume
charge volume
charge pressure
flight data
third-stage servomechanisms
long march 3 series launch vehicle
simulation data
extreme flight condition
mass power
Online Access:https://digital-library.theiet.org/content/journals/10.1049/joe.2020.0069

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https://digital-library.theiet.org/content/journals/10.1049/joe.2020.0069

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