A Review of ETM-03 (A Five Segment Shuttle RSRM Configuration) Ballistic Performance-Reference-Cited by-同舟云学术

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A Review of ETM-03 (A Five Segment Shuttle RSRM Configuration) Ballistic Performance

Published:2004-06-26 Issue: Volume: Page:
ISSN:
Container-title:40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
language:
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Author:

McMillin Joshua¹,Furfaro James¹

Affiliation:

1. ATK Thiokol Propulsion Corp.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-3895

Reference4 articles.

1. 1Huppi, H., Tobias, M., and Seiler, J. "Enhanced Large Solid Rocket Motor Understanding Through Performance Margin Testing RSRM Five-Segment EngineeringTest Motor(ETM-3),"AIAA2003-4958,2003.

2. 2Furfaro,J.A."ErosiveBurningStudyUtilizingUltrasonicMeasurementTechniques,"AIAA2003-4806,2003.

3. 3Wang, Q. "Development of Erosive Burning Models for CFD Prediction of Solid Rocket Motor Internal Environment," AIAA2003-4809,2003.

4. 4Ahmad,R.A.,Morstadt,R.A.,andEaton,A.M."RSRMandETM03InternalFlowSimulationsandComparisons,"AIAA 2003-5104,2003.

Cited by 2 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. Approximate analytical solutions for three-dimensional ascent trajectory of a solid-fuel launch vehicle;Chinese Journal of Aeronautics;2024-06

2. Thrust Oscillations in Reduced Scale Solid Rocket Motors Part I : Experimental Investigations;41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2005-07-10

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