Open Access
| Issue |
JNWPU
Volume 42, Number 1, February 2024
|
|
|---|---|---|
| Page(s) | 108 - 116 | |
| DOI | https://doi.org/10.1051/jnwpu/20244210108 | |
| Published online | 29 March 2024 | |
- GUO Tiancheng. Dynamics of multi-warhead separation process in high speed aerodynamic environment[D]. Harbin: Harbin Institute of Technology, 2019 (in Chinese) [Google Scholar]
- QIAN Cheng, WANG Xiaohui, ZHANG Haizheng, et al. Simulation and analysis of rigid-flexible coupling for stage separation of missile based on ADAMS[J]. Journal of Ordnance Equipment Engineering, 2017(4): 77–81. [Article] (in Chinese) [Google Scholar]
- GU Mingkun, HE Wei, TANG Ke, et al. Research on the development plan of Chinese liquid launch vehicle structure system[J]. Astronautical Systems Engineering Technology, 2021, 5(2): 55–67. [Article] (in Chinese) [Google Scholar]
- CHRISTENSEN K L, NARAHARA R M. Spacecraft separation[J]. Space Aeronuatics, 1996, 46: 74–82 [Google Scholar]
- CHAO J, WANG Z, ZHANG Y. Development of the new approach of formation initialization using spring separation mechanism considering J2 perturbation[J]. Advances in Space Research, 2015, 55(11): 2616–2627. [Article] [CrossRef] [Google Scholar]
- SHIELL J, CANTY P, KILEY A, et al. Dynamic modelling of the bepi-colombo separation system: perturbation analysis of mass properties and separation spring parameters[C]//13th European Space Mechanisms and Tribology Symposium, 2009: 505–532 [Google Scholar]
- LIU Z J, ZHAO X Q, ZHANG J Y, et al. Spiral torsion spring optimization design for separation devices[J]. Journal of Donghua University(English Edition), 2016(2): 33 [Google Scholar]
- YUAN Yong, CHEN Hui, DU Shanliang, et al. Modeling and analysis on separation process for small satellite[J]. Flight Dynamics, 2019, 37(1): 4. [Article] (in Chinese) [Google Scholar]
- GUO Yongchang. Study on interstage scheme of solid launch vehicle considering residual thrust[D]. Harbin: Harbin Institute of Technology, 2017 (in Chinese) [Google Scholar]
- HURLEY M J, CARRIE G W. Stage separation of parallel-staged shuttle vehicles-A capability assessment[J]. Journal of Spacecraft & Rockets, 2012, 9(10): 764–771 [Google Scholar]
- RAO B N, JEYAKUMAR D, BISWAS K K, et al. Rigid body separation dynamics for space launch vehicles[J]. The Aeronautical Journal, 2016, 110(1107): 289–302 [Google Scholar]
- PAMADI B N, TARTABINI P V, TONIOLO M D, et al. Application of constraint force equation methodology for launch vehicle stage separation[J]. Journal of Spacecraft and Rockets, 2013, 50(1): 191–205. [Article] [NASA ADS] [CrossRef] [Google Scholar]
- LI Yanjun. Co-simulation analysis of stage separation of missile based on FLUENT and ADAMS[D]. Harbin: Harbin Institute of Technology, 2012 (in Chinese) [Google Scholar]
- TIAN S, FU J, CHEN J. A numerical method for multi-body separation with collisions[J]. Aerospace Science and Technology, 2020, 109(3): 106426 [Google Scholar]
- ROSHANIAN J, TALEBI M. Monte Carlo simulation of stage separation dynamics of a multistage launch vehicle[J]. Applied Mathematics and Mechanics, 2008(11): 29 [Google Scholar]
- JUNG U H, KIM J H, KIM J H, et al. Optimum design of diffuser in a small high-speed centrifugal fan using CFD & DOE[J]. Journal of Mechanical Science & Technology, 2016, 30(3): 1171–1184 [CrossRef] [Google Scholar]
- LAI Yuyang. Isight parameter optimization theory and example explanation[M]. Beijing: Beihang University Press, 2012: 1–10 (in Chinese) [Google Scholar]
Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.
Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.
Initial download of the metrics may take a while.