The Design of Cylindrical Propellant Grains
Author:
Affiliation:
1. The Glenn L. Martin Co., Baltimore, Md.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.7134
Reference3 articles.
1. Charge Geometry and Ballistic Parameters for Solid Propellant Rocket Motors
Cited by 9 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. Burn-back Equations for High Volumetric Loading Single-grain Dual-thrust Rocket Propellant Configuration;Defence Science Journal;2011-02-11
2. A Geometry Independent Technique for Solid Propellant Grain Design;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;1996-07
3. The Morphological Continuum in Solid Propellant Grain Design;Astrophysics and Space Science Library;1970
4. THE MORPHOLOGICAL CONTINUUM IN SOLID-PROPELLANT GRAIN DESIGN;Propulsion Re-Entry Physics;1970
5. Solid boost thrust decay control for stage separation;3rd Annual Meeting;1966-08-16
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