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Practical Methodology for the Inclusion of Nonlinear Slosh Damping in the Stability Analysis of Liquid Propelled Launch Vehicles
NTRS Full-Text: Click to View  [PDF Size: 1.1 MB]
Author and Affiliation:
Ottander, John(Jacobs Technology Inc., ESSCA, Tullahoma, TN, United States)
Hall, Robert A.(Jacobs Technology Inc., ESSCA, Tullahoma, TN, United States)
Powers, Joseph F.(NASA Marshall Space Flight Center, Huntsville, AL, United States)
Abstract: No abstract available
Publication Date: Jan 08, 2018
Document ID:
20180001121
(Acquired Feb 13, 2018)
Subject Category: LAUNCH VEHICLES AND LAUNCH OPERATIONS; PROPELLANTS AND FUELS
Report/Patent Number: M17-6458
Document Type: Oral/Visual Presentation
Meeting Information: AIAA SciTech Forum; 8-12 Jan. 2018; Kissimmee, FL; United States
Meeting Sponsor: American Inst. of Aeronautics and Astronautics; Reston, VA, United States
Contract/Grant/Task Num: 80MSFC18C0011
Financial Sponsor: NASA Marshall Space Flight Center; Huntsville, AL, United States
Description: 20p; In English
Distribution Limits: Unclassified; Publicly available; Unlimited
Rights: Copyright; Public use permitted
NASA Terms: ATTITUDE CONTROL; DAMPING; EQUATIONS OF MOTION; FLUID DYNAMICS; FLIGHT MECHANICS; LIQUID SLOSHING; NONLINEARITY; PROPELLANT TANKS; SPACECRAFT LAUNCHING; SPACE LAUNCH SYSTEM (SLS); STABILITY TESTS; ACTUATORS; DISPLACEMENT; FREQUENCY RANGES; FREQUENCY DOMAIN ANALYSIS; MATHEMATICAL MODELS; TIME DOMAIN ANALYSIS
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