Multibody Dynamics of Flexible Liquid Rockets with Depleting Propellant-Reference-Cited by-同舟云学术

Multibody Dynamics of Flexible Liquid Rockets with Depleting Propellant

Published:2013-11 Issue:6 Volume:36 Page:1840-1849
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Hu Pengxiang¹,Ren Gexue¹

Affiliation:

1. School of Aerospace, Tsinghua University, 100084 Beijing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.59686

Reference25 articles.

1. RosserJ. B.NewtonR. R.CrossG. L., Mathematical Theory of Rocket Flight, McGraw–Hill, New York, 1947, pp. 1–50.

2. ThomsonW. T., Introduction to Space Dynamics, Wiley, New York, 1963, pp. 230–236.

3. Mechanics of variable mass systems

4. SeideP. “Effect of Constant Longitudinal Acceleration on the Transverse Vibration of Uniform Beams,” Aerospace Corp., Rept. TDR-169(3560-30)-TN-6, Oct. 1963.

Cited by 13 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Transient resonance of sloshing liquid with time-varying mass;Physics of Fluids;2024-06-01

2. Stage separation of recoverable liquid launch vehicle by using moving pulsating ball analogue for propellant sloshing;Chinese Journal of Aeronautics;2024-02

3. Study of Recoverable Liquid Launch Vehicle Stage Separation Based on Equivalent Model of Large-Amplitude Liquid Slosh;Lecture Notes in Mechanical Engineering;2024

4. Equivalent Dynamic of Liquid Sloshing Coupled with Mass Transfer During On-Orbit Refueling;Journal of Spacecraft and Rockets;2023-05

5. Comparison of the Dynamic Characteristics of Electric Pump and Pressure-fed Systems for Space Engines;2022 13th International Conference on Mechanical and Aerospace Engineering (ICMAE);2022-07-20