Future reusable launch vehicles in europe: the FLTP (Future Launchers Technologies Programme)-Reference-Cited by-同舟云学术

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Future reusable launch vehicles in europe: the FLTP (Future Launchers Technologies Programme)

Published:2000-07 Issue:2-9 Volume:47 Page:113-118
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Bonnal Ch.,Caporicci M.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Cited by 8 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. Multidisciplinary design and optimization of winged architectures for reusable launch vehicles;Acta Astronautica;2023-10

2. Dynamic reliability analysis for the reusable thrust chamber: A multi-failure modes investigation based on coupled thermal-structural analysis;Reliability Engineering & System Safety;2020-12

3. Optimal Conceptual Design of Two-Stage Reusable Rocket Vehicles Including Trajectory Optimization;Journal of Spacecraft and Rockets;2004-09

4. A Device for Reduction of Heat Flux Produced by Hypersonic Shock Interference;34th AIAA Fluid Dynamics Conference and Exhibit;2004-06-19

5. CFD Analysis of Aerodynamic Interference Between a Delta Wing and a Hemisphere-Cylinder;42nd AIAA Aerospace Sciences Meeting and Exhibit;2004-01-05

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