Experimental Program to Assess Erosive Burning in Segmented Solid Rocket Motors-Reference-Cited by-同舟云学术

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Experimental Program to Assess Erosive Burning in Segmented Solid Rocket Motors

Published:2007-07-08 Issue: Volume: Page:
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Container-title:43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Heister Stephen,Moss James

Publisher

American Institute of Aeronautics and Astronautics

Reference16 articles.

1. Strand, L., Nguyen, M. H., and Cohen, N. S . "The Scaling of the Threshold Conditions for Solid Propellant Erosive Burning,"AIAA/ASME/SAE/ASEE 24thJoint Propulsion Conf., Boston,MA, AIAAPaper88-3254,July1988.

2. Furfaro, James A, "Erosive BurningStudyUtilizingUltrasonicMeasurement Techniques,"39th AIAA/ASME/SAE/ASEE JointPropulsion Conference, AIAAPaper2003-4806, Huntsville, Alabama, 20-23July2003

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. Development of a hybrid method in a 3-D numerical burn-back analysis for solid propellant grains;Aerospace Science and Technology;2020-11

2. Study of Maximum Pressure Rise with Erosive Burning in Multi‐Grain Tubular Solid Propellant;Propellants, Explosives, Pyrotechnics;2020-07-16

3. Propulsion Educational and Research Programs at Purdue University;43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2007-07-08

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