Aerothermodynamic study of Two-Stage-To-Orbit system composed of wide-speed-range vehicle and rocket-Reference-Cited by-同舟云学术

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Aerothermodynamic study of Two-Stage-To-Orbit system composed of wide-speed-range vehicle and rocket

Published:2021-06 Issue: Volume:183 Page:330-345
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Cheng Jiaming,Chen Rongqian,Qiu Ruofan,Sun Weiqiang,You Yancheng

Funder

Natural Science Foundation of Fujian Province

Fundamental Research Funds for the Central Universities

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference44 articles.

1. History of high-speed flight and its technical development;Anderson;AIAA J.,2001

2. Hypersonic and High-Temperature Gas Dynamics, Vol. 106;Anderson,2006

3. Analysis of the Staging Maneuver and Booster Glideback Guidance for a Two-Stage, Winged, Fully Reusable Launch Vehicle;Naftel,1993

4. Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles;Hirschel,2009

5. Economics of small fully reusable launch systems;Koelle;Acta Astronaut.,1991

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1. Analysis of the aerodynamic performance of a hypersonic gliding missile with a deflected warhead;Physics of Fluids;2024-05-01

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

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

4. Derivation and validation of a similarity law for free-flight wind tunnel tests of parallel stage separation;Chinese Journal of Aeronautics;2023-08

5. Effects of expansion waves on incident shock-wave/boundary-layer interactions in hypersonic flows;Physics of Fluids;2023-05-01

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