Unsteady interaction mechanism of transverse stage separation in hypersonic flow for a two-stage-to-orbit vehicle
Due to the complex aerodynamic interaction, the safe separation of two stages is one of the
challenges for the successful launch of a two-stage-to-orbit (TSTO) vehicle. The unsteady …
challenges for the successful launch of a two-stage-to-orbit (TSTO) vehicle. The unsteady …
Unsteady interaction and dynamic stability analysis of a two-stage-to-orbit vehicle during transverse stage separation
Y Wang, Y Wang - Acta Astronautica, 2024 - Elsevier
Hypersonic stage separation is a significant process for the future two-stage-to-orbit (TSTO)
vehicle. Strong and complex interstage aerodynamic interference may result in drastic …
vehicle. Strong and complex interstage aerodynamic interference may result in drastic …
Experimental and numerical investigation on the unsteady interaction in longitudinal stage separation for parallel-staged two-body configuration
Hypersonic stage separation is a significant process, probably involving complex
aerodynamic interaction, which determines the survival of two-stage-to-orbit (TSTO) …
aerodynamic interaction, which determines the survival of two-stage-to-orbit (TSTO) …
[PDF][PDF] 激波风洞两级入轨飞行器纵向级间分离试验技术
王粤， 汪运鹏， 姜宗林 - Acta Aeronautica et Astronautica Sinica, 2023 - researchgate.net
高超声速多体分离问题是航天多体飞行器研发中的关键技术问题, 基于分离过程中高速流动的
复杂性, 对高速多体分离的风洞试验研究极具挑战性, 特别是激波风洞分离试验 …
复杂性, 对高速多体分离的风洞试验研究极具挑战性, 特别是激波风洞分离试验 …
Precise control of interstage separation attitude of two-stage-to-orbit vehicle
Q JIANG, C Shusheng, Y Hua, LI Zuotai… - Acta Aeronautica et …, 2024 - sciopen.com
Precise attitude control of the orbiter and the booster is particularly important for the
interstage separation of the Two-Stage-to-Orbit (TSTO) vehicle. Numerical simulation can …
interstage separation of the Two-Stage-to-Orbit (TSTO) vehicle. Numerical simulation can …
The Numerical and Experimental Research on Supersonic Parallel Separation
H Qin, F Xie, L Chen, F Wang - Asia-Pacific International Symposium on …, 2023 - Springer
There is a very complex flow structure between two parallel arrangement lifting body
vehicles and the structure changes rapidly with the relative position and attitude. The …
vehicles and the structure changes rapidly with the relative position and attitude. The …
[引用][C] 극초음속비행체형상파라미터연구
이학민， 박상현， 최재훈， 박영민 - 한국항공우주학회학술발표회초록집, 2023 - dbpia.co.kr
한국항공우주연구원에서는 기본사업인 극초음속 비행체 핵심기술 과제를 년부터 수행하고
있다 극 2022. 초음속 비행체 복합엔진 축소형 기술 시현 극초음속, 비행체 고온 열보호시스템 …
있다 극 2022. 초음속 비행체 복합엔진 축소형 기술 시현 극초음속, 비행체 고온 열보호시스템 …