Hypersonic aerodynamic interference investigation for a two-stage-to-orbit model-Reference-Cited by-同舟云学术

Hypersonic aerodynamic interference investigation for a two-stage-to-orbit model

Published:2020-03 Issue: Volume:168 Page:138-145
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Jia Juhong^ORCID,Fu Debin,He Zepeng,Yang Junfan,Hu Lijie

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference31 articles.

1. Comprehensive design of uniform robust exact disturbance observer and fixed-time controller for reusable launch vehicles;You;IET Control Theory & Appl.,2018

2. Adaptive fault-tolerant control for a VTVL reusable launch vehicle;Zhang;Acta Astronaut.,2019

3. System design of a reusable, horizontal take-off/horizontal landing two stage to orbit vehicle;Griesemer;46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit,2010

4. Economics of small fully reusable launch systems (SSTO vs. TSTO);Koelle;Acta Astronaut.,1997

5. Review on active thermal protection and its heat transfer for airbreathing hypersonic vehicles;Zhu;Chin. J. Aeronaut.,2018

Cited by 20 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. Unsteady interaction and dynamic stability analysis of a two-stage-to-orbit vehicle during transverse stage separation;Acta Astronautica;2024-03

2. The Numerical and Experimental Research on Supersonic Parallel Separation;Lecture Notes in Electrical Engineering;2024

3. A stability-enhanced approach for aerodynamic heating computation in high-speed flows;Journal of Physics: Conference Series;2024-01-01

4. Unsteady investigation on parallel separation for spiked two-stage reusable launch vehicle;Chinese Journal of Aeronautics;2023-11

5. A Study on Flow and Aerodynamic Characteristics During Separation Stage of Hypersonic Launch Vehicle on Level Flight;Journal of the Korean Society for Aeronautical & Space Sciences;2023-10-31