Dynamic Analysis of Internally Carried Air-launched Launch Vehicle Separation from Aircraft Based on ADAMS

ZHANG  Jiuxing; ZHANG  Dengcheng; ZHU  Hequan; ZHANG  Yanhua

doi:10.15892/j.cnki.djzdxb.2011.02.039

Journal of Projectiles, Rockets, Missiles and Guidance >

2011 , Vol. 31 >Issue 2: 153 - 156

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2011.02.039

BALLISTIC AND AIRDYNAMICS

Dynamic Analysis of Internally Carried Air-launched Launch Vehicle Separation from Aircraft Based on ADAMS

ZHANG Jiuxing ,
ZHANG Dengcheng ,
ZHU Hequan ,
ZHANG Yanhua

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The Engineering Institute, Air Force Engineering University, Xi'an 710038, China

Received date: 2010-05-22

Online published: 2025-05-30

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Abstract

In order to verify the total project of internally carried air-launched launch vehicle, the physical models of the cargo, launch vehicle and parachute based on ADAMS and Solidworks were built. The dynamic equation for the dynamic simulation was built according to the detailed dynamic analysis of the three in the process of separation. The simulation model is proved correctly according to the dynamic simulation; it provides a new reference method for air dynamic simulation.

Key words： ADAMS; dynamic analysis; flight dynamics; air launch; launch vehicle; parachute and payload system

Cite this article

ZHANG Jiuxing , ZHANG Dengcheng , ZHU Hequan , ZHANG Yanhua . Dynamic Analysis of Internally Carried Air-launched Launch Vehicle Separation from Aircraft Based on ADAMS[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2011 , 31(2) : 153 -156 . DOI: 10.15892/j.cnki.djzdxb.2011.02.039

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