The Design of Cylindrical Propellant Grains

Author:

EPSTEIN L. IVAN1

Affiliation:

1. The Glenn L. Martin Co., Baltimore, Md.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

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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