New Concept for Weight Optimization of Launcher Nose Firings Made of Honeycomb Structures
Author:
Affiliation:
1. Research Institute of Engineering Technique OJSC, Dnipropetrovsk, Ukraine
2. N. E. Zhukovsky National Aerospace University (Kharkov Aviation Institute), Kharkov, Ukraine
3. NITOM Scientific and Production Enterprise, Dnipropetrovsk, Ukraine
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.IAC-06-C2.P.1.11
Cited by 6 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. Optimal Design of Composite Shelled Sandwich Structures with a Honeycomb Filler;Lecture Notes in Mechanical Engineering;2021
2. Analysis of the Bearing Capacity of Adhesive Joint of Honeycomb Cores of Sandwich Structures with the Continuous Adhesive Layer;Key Engineering Materials;2020-09
3. Improving the mass efficiency of a composite launch vehicle head fairing with a sandwich structure;Eastern-European Journal of Enterprise Technologies;2019-11-21
4. Effect of technological camber in the facets of a cellular filler on its physical and mechanical characteristics;Eastern-European Journal of Enterprise Technologies;2019-09-30
5. Weight-based optimization of sandwich shelled composite structures with a honeycomb filler;Eastern-European Journal of Enterprise Technologies;2019-01-22
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