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Construction of Supersonic Flight Dynamics Test (SFDT-2) Vehicle Monte Carlo Splashdown Footprints for Use in Range Safety and Recovery PlanningOverview of Low Density Supersonic Decelerator (LDSD) SFDT-2 ( Supersonic Flight Dynamics Test-2) flight profile; Description of Monte Carlo flight dynamics simulations performed; Modeling and uncertainties; Results with statistical prediction of test vehicle splashdown location; Use of Monte Carlo results for range safety and recovery planning.
Document ID
20190026930
Acquisition Source
Jet Propulsion Laboratory
Document Type
Presentation
External Source(s)
hdl:2014/46327
Authors
Strauss, Bill (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Ivanov, Mark (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
July 1, 2019
Publication Date
February 15, 2016
Subject Category
Launch Vehicles And Launch Operations
Ground Support Systems And Facilities (Space)
Report/Patent Number
JPL-CL-16-0595
Report Number: JPL-CL-16-0595
Meeting Information
Meeting: AAS/AIAA Space Flight Mechanics Meeting
Location: Napa, CA
Country: United States
Start Date: February 14, 2016
End Date: February 18, 2016
Sponsors: American Astronautical Society (AAS-HQ), American Institute of Aeronautics and Astronautics (AIAA)
Distribution Limits
Public
Copyright
Other

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