Determination of the interior ballistic properties of solid propellants from progressive burning grains data.
Author:
Affiliation:
1. Ministry of Defence, Tel Aviv, Israel
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.29320
Reference3 articles.
1. A conformal mapping method to predict low-speed aerodynamic characteristics of arbitrary slender re-entry shapes.
2. Calculation of stability derivatives by slender-body theory.
Cited by 3 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. Performance Prediction of BPN Pyrogen-Type Igniters for Rocket Motors;Journal of Spacecraft and Rockets;1977-04
2. Performance prediction of BPN pyrogen-type igniters for rocket motors;12th Propulsion Conference;1976-07-26
3. Investigation of high pressure burning characteristics of composite solid propellants;5th Propulsion Joint Specialist;1969-06-09
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