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Dynamic Analysis of Sounding Rocket Pneumatic System RevisionThe recent fusion of decades of advancements in mathematical models, numerical algorithms and curve fitting techniques marked the beginning of a new era in the science of simulation. It is becoming indispensable to the study of rockets and aerospace analysis. In pneumatic system, which is the main focus of this paper, particular emphasis will be placed on the efforts of compressible flow in Attitude Control System of sounding rocket.
Document ID
20110007991
Acquisition Source
Goddard Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Armen, Jerald (Northrop Grumman Space Technologies Greenbelt, MD, United States)
Date Acquired
August 25, 2013
Publication Date
June 8, 2010
Subject Category
Fluid Mechanics And Thermodynamics
Distribution Limits
Public
Copyright
Public Use Permitted.

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